Sample records for taguchi robust design

  1. Incorporating Servqual-QFD with Taguchi Design for optimizing service quality design

    NASA Astrophysics Data System (ADS)

    Arbi Hadiyat, M.

    2018-03-01

    Deploying good service design in service companies has been updated issue in improving customer satisfaction, especially based on the level of service quality measured by Parasuraman’s SERVQUAL. Many researchers have been proposing methods in designing the service, and some of them are based on engineering viewpoint, especially by implementing the QFD method or even using robust Taguchi method. The QFD method would found the qualitative solution by generating the “how’s”, while Taguchi method gives more quantitative calculation in optimizing best solution. However, incorporating both QFD and Taguchi has been done in this paper and yields better design process. The purposes of this research is to evaluate the incorporated methods by implemented it to a case study, then analyze the result and see the robustness of those methods to customer perception of service quality. Started by measuring service attributes using SERVQUAL and find the improvement with QFD, the deployment of QFD solution then generated by defining Taguchi factors levels and calculating the Signal-to-noise ratio in its orthogonal array, and optimized Taguchi response then found. A case study was given for designing service in local bank. Afterward, the service design obtained from previous analysis was then evaluated and shows that it was still meet the customer satisfaction. Incorporating QFD and Taguchi has performed well and can be adopted and developed for another research for evaluating the robustness of result.

  2. Optimal design of loudspeaker arrays for robust cross-talk cancellation using the Taguchi method and the genetic algorithm.

    PubMed

    Bai, Mingsian R; Tung, Chih-Wei; Lee, Chih-Chung

    2005-05-01

    An optimal design technique of loudspeaker arrays for cross-talk cancellation with application in three-dimensional audio is presented. An array focusing scheme is presented on the basis of the inverse propagation that relates the transducers to a set of chosen control points. Tikhonov regularization is employed in designing the inverse cancellation filters. An extensive analysis is conducted to explore the cancellation performance and robustness issues. To best compromise the performance and robustness of the cross-talk cancellation system, optimal configurations are obtained with the aid of the Taguchi method and the genetic algorithm (GA). The proposed systems are further justified by physical as well as subjective experiments. The results reveal that large number of loudspeakers, closely spaced configuration, and optimal control point design all contribute to the robustness of cross-talk cancellation systems (CCS) against head misalignment.

  3. Taguchi experimental design to determine the taste quality characteristic of candied carrot

    NASA Astrophysics Data System (ADS)

    Ekawati, Y.; Hapsari, A. A.

    2018-03-01

    Robust parameter design is used to design product that is robust to noise factors so the product’s performance fits the target and delivers a better quality. In the process of designing and developing the innovative product of candied carrot, robust parameter design is carried out using Taguchi Method. The method is used to determine an optimal quality design. The optimal quality design is based on the process and the composition of product ingredients that are in accordance with consumer needs and requirements. According to the identification of consumer needs from the previous research, quality dimensions that need to be assessed are the taste and texture of the product. The quality dimension assessed in this research is limited to the taste dimension. Organoleptic testing is used for this assessment, specifically hedonic testing that makes assessment based on consumer preferences. The data processing uses mean and signal to noise ratio calculation and optimal level setting to determine the optimal process/composition of product ingredients. The optimal value is analyzed using confirmation experiments to prove that proposed product match consumer needs and requirements. The result of this research is identification of factors that affect the product taste and the optimal quality of product according to Taguchi Method.

  4. Taguchi method of experimental design in materials education

    NASA Technical Reports Server (NTRS)

    Weiser, Martin W.

    1993-01-01

    Some of the advantages and disadvantages of the Taguchi Method of experimental design as applied to Materials Science will be discussed. This is a fractional factorial method that employs the minimum number of experimental trials for the information obtained. The analysis is also very simple to use and teach, which is quite advantageous in the classroom. In addition, the Taguchi loss function can be easily incorporated to emphasize that improvements in reproducibility are often at least as important as optimization of the response. The disadvantages of the Taguchi Method include the fact that factor interactions are normally not accounted for, there are zero degrees of freedom if all of the possible factors are used, and randomization is normally not used to prevent environmental biasing. In spite of these disadvantages it is felt that the Taguchi Method is extremely useful for both teaching experimental design and as a research tool, as will be shown with a number of brief examples.

  5. Robust design of microchannel cooler

    NASA Astrophysics Data System (ADS)

    He, Ye; Yang, Tao; Hu, Li; Li, Leimin

    2005-12-01

    Microchannel cooler has offered a new method for the cooling of high power diode lasers, with the advantages of small volume, high efficiency of thermal dissipation and low cost when mass-produced. In order to reduce the sensitivity of design to manufacture errors or other disturbances, Taguchi method that is one of robust design method was chosen to optimize three parameters important to the cooling performance of roof-like microchannel cooler. The hydromechanical and thermal mathematical model of varying section microchannel was calculated using finite volume method by FLUENT. A special program was written to realize the automation of the design process for improving efficiency. The optimal design is presented which compromises between optimal cooling performance and its robustness. This design method proves to be available.

  6. Assessing the applicability of the Taguchi design method to an interrill erosion study

    NASA Astrophysics Data System (ADS)

    Zhang, F. B.; Wang, Z. L.; Yang, M. Y.

    2015-02-01

    Full-factorial experimental designs have been used in soil erosion studies, but are time, cost and labor intensive, and sometimes they are impossible to conduct due to the increasing number of factors and their levels to consider. The Taguchi design is a simple, economical and efficient statistical tool that only uses a portion of the total possible factorial combinations to obtain the results of a study. Soil erosion studies that use the Taguchi design are scarce and no comparisons with full-factorial designs have been made. In this paper, a series of simulated rainfall experiments using a full-factorial design of five slope lengths (0.4, 0.8, 1.2, 1.6, and 2 m), five slope gradients (18%, 27%, 36%, 48%, and 58%), and five rainfall intensities (48, 62.4, 102, 149, and 170 mm h-1) were conducted. Validation of the applicability of a Taguchi design to interrill erosion experiments was achieved by extracting data from the full dataset according to a theoretical Taguchi design. The statistical parameters for the mean quasi-steady state erosion and runoff rates of each test, the optimum conditions for producing maximum erosion and runoff, and the main effect and percentage contribution of each factor obtained from the full-factorial and Taguchi designs were compared. Both designs generated almost identical results. Using the experimental data from the Taguchi design, it was possible to accurately predict the erosion and runoff rates under the conditions that had been excluded from the Taguchi design. All of the results obtained from analyzing the experimental data for both designs indicated that the Taguchi design could be applied to interrill erosion studies and could replace full-factorial designs. This would save time, labor and costs by generally reducing the number of tests to be conducted. Further work should test the applicability of the Taguchi design to a wider range of conditions.

  7. Simulation reduction using the Taguchi method

    NASA Technical Reports Server (NTRS)

    Mistree, Farrokh; Lautenschlager, Ume; Erikstad, Stein Owe; Allen, Janet K.

    1993-01-01

    A large amount of engineering effort is consumed in conducting experiments to obtain information needed for making design decisions. Efficiency in generating such information is the key to meeting market windows, keeping development and manufacturing costs low, and having high-quality products. The principal focus of this project is to develop and implement applications of Taguchi's quality engineering techniques. In particular, we show how these techniques are applied to reduce the number of experiments for trajectory simulation of the LifeSat space vehicle. Orthogonal arrays are used to study many parameters simultaneously with a minimum of time and resources. Taguchi's signal to noise ratio is being employed to measure quality. A compromise Decision Support Problem and Robust Design are applied to demonstrate how quality is designed into a product in the early stages of designing.

  8. Thermochemical hydrolysis of macroalgae Ulva for biorefinery: Taguchi robust design method

    NASA Astrophysics Data System (ADS)

    Jiang, Rui; Linzon, Yoav; Vitkin, Edward; Yakhini, Zohar; Chudnovsky, Alexandra; Golberg, Alexander

    2016-06-01

    Understanding the impact of all process parameters on the efficiency of biomass hydrolysis and on the final yield of products is critical to biorefinery design. Using Taguchi orthogonal arrays experimental design and Partial Least Square Regression, we investigated the impact of change and the comparative significance of thermochemical process temperature, treatment time, %Acid and %Solid load on carbohydrates release from green macroalgae from Ulva genus, a promising biorefinery feedstock. The average density of hydrolysate was determined using a new microelectromechanical optical resonator mass sensor. In addition, using Flux Balance Analysis techniques, we compared the potential fermentation yields of these hydrolysate products using metabolic models of Escherichia coli, Saccharomyces cerevisiae wild type, Saccharomyces cerevisiae RN1016 with xylose isomerase and Clostridium acetobutylicum. We found that %Acid plays the most significant role and treatment time the least significant role in affecting the monosaccharaides released from Ulva biomass. We also found that within the tested range of parameters, hydrolysis with 121 °C, 30 min 2% Acid, 15% Solids could lead to the highest yields of conversion: 54.134-57.500 gr ethanol kg-1 Ulva dry weight by S. cerevisiae RN1016 with xylose isomerase. Our results support optimized marine algae utilization process design and will enable smart energy harvesting by thermochemical hydrolysis.

  9. Optimization of Tape Winding Process Parameters to Enhance the Performance of Solid Rocket Nozzle Throat Back Up Liners using Taguchi's Robust Design Methodology

    NASA Astrophysics Data System (ADS)

    Nath, Nayani Kishore

    2017-08-01

    The throat back up liners is used to protect the nozzle structural members from the severe thermal environment in solid rocket nozzles. The throat back up liners is made with E-glass phenolic prepregs by tape winding process. The objective of this work is to demonstrate the optimization of process parameters of tape winding process to achieve better insulative resistance using Taguchi's robust design methodology. In this method four control factors machine speed, roller pressure, tape tension, tape temperature that were investigated for the tape winding process. The presented work was to study the cogency and acceptability of Taguchi's methodology in manufacturing of throat back up liners. The quality characteristic identified was Back wall temperature. Experiments carried out using L 9 ' (34) orthogonal array with three levels of four different control factors. The test results were analyzed using smaller the better criteria for Signal to Noise ratio in order to optimize the process. The experimental results were analyzed conformed and successfully used to achieve the minimum back wall temperature of the throat back up liners. The enhancement in performance of the throat back up liners was observed by carrying out the oxy-acetylene tests. The influence of back wall temperature on the performance of throat back up liners was verified by ground firing test.

  10. Thermochemical hydrolysis of macroalgae Ulva for biorefinery: Taguchi robust design method

    PubMed Central

    Jiang, Rui; Linzon, Yoav; Vitkin, Edward; Yakhini, Zohar; Chudnovsky, Alexandra; Golberg, Alexander

    2016-01-01

    Understanding the impact of all process parameters on the efficiency of biomass hydrolysis and on the final yield of products is critical to biorefinery design. Using Taguchi orthogonal arrays experimental design and Partial Least Square Regression, we investigated the impact of change and the comparative significance of thermochemical process temperature, treatment time, %Acid and %Solid load on carbohydrates release from green macroalgae from Ulva genus, a promising biorefinery feedstock. The average density of hydrolysate was determined using a new microelectromechanical optical resonator mass sensor. In addition, using Flux Balance Analysis techniques, we compared the potential fermentation yields of these hydrolysate products using metabolic models of Escherichia coli, Saccharomyces cerevisiae wild type, Saccharomyces cerevisiae RN1016 with xylose isomerase and Clostridium acetobutylicum. We found that %Acid plays the most significant role and treatment time the least significant role in affecting the monosaccharaides released from Ulva biomass. We also found that within the tested range of parameters, hydrolysis with 121 °C, 30 min 2% Acid, 15% Solids could lead to the highest yields of conversion: 54.134–57.500 gr ethanol kg−1 Ulva dry weight by S. cerevisiae RN1016 with xylose isomerase. Our results support optimized marine algae utilization process design and will enable smart energy harvesting by thermochemical hydrolysis. PMID:27291594

  11. A Taguchi study of the aeroelastic tailoring design process

    NASA Technical Reports Server (NTRS)

    Bohlmann, Jonathan D.; Scott, Robert C.

    1991-01-01

    A Taguchi study was performed to determine the important players in the aeroelastic tailoring design process and to find the best composition of the optimization's objective function. The Wing Aeroelastic Synthesis Procedure (TSO) was used to ascertain the effects that factors such as composite laminate constraints, roll effectiveness constraints, and built-in wing twist and camber have on the optimum, aeroelastically tailored wing skin design. The results show the Taguchi method to be a viable engineering tool for computational inquiries, and provide some valuable lessons about the practice of aeroelastic tailoring.

  12. Permeability Evaluation Through Chitosan Membranes Using Taguchi Design

    PubMed Central

    Sharma, Vipin; Marwaha, Rakesh Kumar; Dureja, Harish

    2010-01-01

    In the present study, chitosan membranes capable of imitating permeation characteristics of diclofenac diethylamine across animal skin were prepared using cast drying method. The effect of concentration of chitosan, concentration of cross-linking agent (NaTPP), crosslinking time was studied using Taguchi design. Taguchi design ranked concentration of chitosan as the most important factor influencing the permeation parameters of diclofenac diethylamine. The flux of the diclofenac diethylamine solution through optimized chitosan membrane (T9) was found to be comparable to that obtained across rat skin. The mathematical model developed using multilinear regression analysis can be used to formulate chitosan membranes that can mimic the desired permeation characteristics. The developed chitosan membranes can be utilized as a substitute to animal skin for in vitro permeation studies. PMID:21179329

  13. Permeability evaluation through chitosan membranes using taguchi design.

    PubMed

    Sharma, Vipin; Marwaha, Rakesh Kumar; Dureja, Harish

    2010-01-01

    In the present study, chitosan membranes capable of imitating permeation characteristics of diclofenac diethylamine across animal skin were prepared using cast drying method. The effect of concentration of chitosan, concentration of cross-linking agent (NaTPP), crosslinking time was studied using Taguchi design. Taguchi design ranked concentration of chitosan as the most important factor influencing the permeation parameters of diclofenac diethylamine. The flux of the diclofenac diethylamine solution through optimized chitosan membrane (T9) was found to be comparable to that obtained across rat skin. The mathematical model developed using multilinear regression analysis can be used to formulate chitosan membranes that can mimic the desired permeation characteristics. The developed chitosan membranes can be utilized as a substitute to animal skin for in vitro permeation studies.

  14. Application of Taguchi methods to infrared window design

    NASA Astrophysics Data System (ADS)

    Osmer, Kurt A.; Pruszynski, Charles J.

    1990-10-01

    Dr. Genichi Taguchi, a prominent quality consultant, reduced a branch of statistics known as "Design of Experiments" to a cookbook methodology that can be employed by any competent engineer. This technique has been extensively employed by Japanese manufacturers, and is widely credited with helping them attain their current level of success in low cost, high quality product design and fabrication. Although this technique was originally put forth as a tool to streamline the determination of improved production processes, it can also be applied to a wide range of engineering problems. As part of an internal research project, this method of experimental design has been adapted to window trade studies and materials research. Two of these analyses are presented herein, and have been chosen to illustrate the breadth of applications to which the Taguchi method can be utilized.

  15. Taguchi Approach to Design Optimization for Quality and Cost: An Overview

    NASA Technical Reports Server (NTRS)

    Unal, Resit; Dean, Edwin B.

    1990-01-01

    Calibrations to existing cost of doing business in space indicate that to establish human presence on the Moon and Mars with the Space Exploration Initiative (SEI) will require resources, felt by many, to be more than the national budget can afford. In order for SEI to succeed, we must actually design and build space systems at lower cost this time, even with tremendous increases in quality and performance requirements, such as extremely high reliability. This implies that both government and industry must change the way they do business. Therefore, new philosophy and technology must be employed to design and produce reliable, high quality space systems at low cost. In recognizing the need to reduce cost and improve quality and productivity, Department of Defense (DoD) and National Aeronautics and Space Administration (NASA) have initiated Total Quality Management (TQM). TQM is a revolutionary management strategy in quality assurance and cost reduction. TQM requires complete management commitment, employee involvement, and use of statistical tools. The quality engineering methods of Dr. Taguchi, employing design of experiments (DOE), is one of the most important statistical tools of TQM for designing high quality systems at reduced cost. Taguchi methods provide an efficient and systematic way to optimize designs for performance, quality, and cost. Taguchi methods have been used successfully in Japan and the United States in designing reliable, high quality products at low cost in such areas as automobiles and consumer electronics. However, these methods are just beginning to see application in the aerospace industry. The purpose of this paper is to present an overview of the Taguchi methods for improving quality and reducing cost, describe the current state of applications and its role in identifying cost sensitive design parameters.

  16. Robust modular product family design

    NASA Astrophysics Data System (ADS)

    Jiang, Lan; Allada, Venkat

    2001-10-01

    This paper presents a modified Taguchi methodology to improve the robustness of modular product families against changes in customer requirements. The general research questions posed in this paper are: (1) How to effectively design a product family (PF) that is robust enough to accommodate future customer requirements. (2) How far into the future should designers look to design a robust product family? An example of a simplified vacuum product family is used to illustrate our methodology. In the example, customer requirements are selected as signal factors; future changes of customer requirements are selected as noise factors; an index called quality characteristic (QC) is set to evaluate the product vacuum family; and the module instance matrix (M) is selected as control factor. Initially a relation between the objective function (QC) and the control factor (M) is established, and then the feasible M space is systemically explored using a simplex method to determine the optimum M and the corresponding QC values. Next, various noise levels at different time points are introduced into the system. For each noise level, the optimal values of M and QC are computed and plotted on a QC-chart. The tunable time period of the control factor (the module matrix, M) is computed using the QC-chart. The tunable time period represents the maximum time for which a given control factor can be used to satisfy current and future customer needs. Finally, a robustness index is used to break up the tunable time period into suitable time periods that designers should consider while designing product families.

  17. A Gradient Taguchi Method for Engineering Optimization

    NASA Astrophysics Data System (ADS)

    Hwang, Shun-Fa; Wu, Jen-Chih; He, Rong-Song

    2017-10-01

    To balance the robustness and the convergence speed of optimization, a novel hybrid algorithm consisting of Taguchi method and the steepest descent method is proposed in this work. Taguchi method using orthogonal arrays could quickly find the optimum combination of the levels of various factors, even when the number of level and/or factor is quite large. This algorithm is applied to the inverse determination of elastic constants of three composite plates by combining numerical method and vibration testing. For these problems, the proposed algorithm could find better elastic constants in less computation cost. Therefore, the proposed algorithm has nice robustness and fast convergence speed as compared to some hybrid genetic algorithms.

  18. Design of a robust fuzzy controller for the arc stability of CO(2) welding process using the Taguchi method.

    PubMed

    Kim, Dongcheol; Rhee, Sehun

    2002-01-01

    CO(2) welding is a complex process. Weld quality is dependent on arc stability and minimizing the effects of disturbances or changes in the operating condition commonly occurring during the welding process. In order to minimize these effects, a controller can be used. In this study, a fuzzy controller was used in order to stabilize the arc during CO(2) welding. The input variable of the controller was the Mita index. This index estimates quantitatively the arc stability that is influenced by many welding process parameters. Because the welding process is complex, a mathematical model of the Mita index was difficult to derive. Therefore, the parameter settings of the fuzzy controller were determined by performing actual control experiments without using a mathematical model of the controlled process. The solution, the Taguchi method was used to determine the optimal control parameter settings of the fuzzy controller to make the control performance robust and insensitive to the changes in the operating conditions.

  19. Application of Taguchi L32 orthogonal array design to optimize copper biosorption by using Spaghnum moss.

    PubMed

    Ozdemir, Utkan; Ozbay, Bilge; Ozbay, Ismail; Veli, Sevil

    2014-09-01

    In this work, Taguchi L32 experimental design was applied to optimize biosorption of Cu(2+) ions by an easily available biosorbent, Spaghnum moss. With this aim, batch biosorption tests were performed to achieve targeted experimental design with five factors (concentration, pH, biosorbent dosage, temperature and agitation time) at two different levels. Optimal experimental conditions were determined by calculated signal-to-noise ratios. "Higher is better" approach was followed to calculate signal-to-noise ratios as it was aimed to obtain high metal removal efficiencies. The impact ratios of factors were determined by the model. Within the study, Cu(2+) biosorption efficiencies were also predicted by using Taguchi method. Results of the model showed that experimental and predicted values were close to each other demonstrating the success of Taguchi approach. Furthermore, thermodynamic, isotherm and kinetic studies were performed to explain the biosorption mechanism. Calculated thermodynamic parameters were in good accordance with the results of Taguchi model. Copyright © 2014 Elsevier Inc. All rights reserved.

  20. Rapid development of xylanase assay conditions using Taguchi methodology.

    PubMed

    Prasad Uday, Uma Shankar; Bandyopadhyay, Tarun Kanti; Bhunia, Biswanath

    2016-11-01

    The present investigation is mainly concerned with the rapid development of extracellular xylanase assay conditions by using Taguchi methodology. The extracellular xylanase was produced from Aspergillus niger (KP874102.1), a new strain isolated from a soil sample of the Baramura forest, Tripura West, India. Four physical parameters including temperature, pH, buffer concentration and incubation time were considered as key factors for xylanase activity and were optimized using Taguchi robust design methodology for enhanced xylanase activity. The main effect, interaction effects and optimal levels of the process factors were determined using signal-to-noise (S/N) ratio. The Taguchi method recommends the use of S/N ratio to measure quality characteristics. Based on analysis of the S/N ratio, optimal levels of the process factors were determined. Analysis of variance (ANOVA) was performed to evaluate statistically significant process factors. ANOVA results showed that temperature contributed the maximum impact (62.58%) on xylanase activity, followed by pH (22.69%), buffer concentration (9.55%) and incubation time (5.16%). Predicted results showed that enhanced xylanase activity (81.47%) can be achieved with pH 2, temperature 50°C, buffer concentration 50 Mm and incubation time 10 min.

  1. The Taguchi methodology as a statistical tool for biotechnological applications: a critical appraisal.

    PubMed

    Rao, Ravella Sreenivas; Kumar, C Ganesh; Prakasham, R Shetty; Hobbs, Phil J

    2008-04-01

    Success in experiments and/or technology mainly depends on a properly designed process or product. The traditional method of process optimization involves the study of one variable at a time, which requires a number of combinations of experiments that are time, cost and labor intensive. The Taguchi method of design of experiments is a simple statistical tool involving a system of tabulated designs (arrays) that allows a maximum number of main effects to be estimated in an unbiased (orthogonal) fashion with a minimum number of experimental runs. It has been applied to predict the significant contribution of the design variable(s) and the optimum combination of each variable by conducting experiments on a real-time basis. The modeling that is performed essentially relates signal-to-noise ratio to the control variables in a 'main effect only' approach. This approach enables both multiple response and dynamic problems to be studied by handling noise factors. Taguchi principles and concepts have made extensive contributions to industry by bringing focused awareness to robustness, noise and quality. This methodology has been widely applied in many industrial sectors; however, its application in biological sciences has been limited. In the present review, the application and comparison of the Taguchi methodology has been emphasized with specific case studies in the field of biotechnology, particularly in diverse areas like fermentation, food processing, molecular biology, wastewater treatment and bioremediation.

  2. Taguchi Method Applied in Optimization of Shipley SJR 5740 Positive Resist Deposition

    NASA Technical Reports Server (NTRS)

    Hui, A.; Blosiu, J. O.; Wiberg, D. V.

    1998-01-01

    Taguchi Methods of Robust Design presents a way to optimize output process performance through an organized set of experiments by using orthogonal arrays. Analysis of variance and signal-to-noise ratio is used to evaluate the contribution of each of the process controllable parameters in the realization of the process optimization. In the photoresist deposition process, there are numerous controllable parameters that can affect the surface quality and thickness of the final photoresist layer.

  3. Taguchi Based Performance and Reliability Improvement of an Ion Chamber Amplifier for Enhanced Nuclear Reactor Safety

    NASA Astrophysics Data System (ADS)

    Kulkarni, R. D.; Agarwal, Vivek

    2008-08-01

    An ion chamber amplifier (ICA) is used as a safety device for neutronic power (flux) measurement in regulation and protection systems of nuclear reactors. Therefore, performance reliability of an ICA is an important issue. Appropriate quality engineering is essential to achieve a robust design and performance of the ICA circuit. It is observed that the low input bias current operational amplifiers used in the input stage of the ICA circuit are the most critical devices for proper functioning of the ICA. They are very sensitive to the gamma radiation present in their close vicinity. Therefore, the response of the ICA deteriorates with exposure to gamma radiation resulting in a decrease in the overall reliability, unless desired performance is ensured under all conditions. This paper presents a performance enhancement scheme for an ICA operated in the nuclear environment. The Taguchi method, which is a proven technique for reliability enhancement, has been used in this work. It is demonstrated that if a statistical, optimal design approach, like the Taguchi method is used, the cost of high quality and reliability may be brought down drastically. The complete methodology and statistical calculations involved are presented, as are the experimental and simulation results to arrive at a robust design of the ICA.

  4. Dysprosium sorption by polymeric composite bead: robust parametric optimization using Taguchi method.

    PubMed

    Yadav, Kartikey K; Dasgupta, Kinshuk; Singh, Dhruva K; Varshney, Lalit; Singh, Harvinderpal

    2015-03-06

    Polyethersulfone-based beads encapsulating di-2-ethylhexyl phosphoric acid have been synthesized and evaluated for the recovery of rare earth values from the aqueous media. Percentage recovery and the sorption behavior of Dy(III) have been investigated under wide range of experimental parameters using these beads. Taguchi method utilizing L-18 orthogonal array has been adopted to identify the most influential process parameters responsible for higher degree of recovery with enhanced sorption of Dy(III) from chloride medium. Analysis of variance indicated that the feed concentration of Dy(III) is the most influential factor for equilibrium sorption capacity, whereas aqueous phase acidity influences the percentage recovery most. The presence of polyvinyl alcohol and multiwalled carbon nanotube modified the internal structure of the composite beads and resulted in uniform distribution of organic extractant inside polymeric matrix. The experiment performed under optimum process conditions as predicted by Taguchi method resulted in enhanced Dy(III) recovery and sorption capacity by polymeric beads with minimum standard deviation. Copyright © 2015 Elsevier B.V. All rights reserved.

  5. Multidisciplinary design of a rocket-based combined cycle SSTO launch vehicle using Taguchi methods

    NASA Technical Reports Server (NTRS)

    Olds, John R.; Walberg, Gerald D.

    1993-01-01

    Results are presented from the optimization process of a winged-cone configuration SSTO launch vehicle that employs a rocket-based ejector/ramjet/scramjet/rocket operational mode variable-cycle engine. The Taguchi multidisciplinary parametric-design method was used to evaluate the effects of simultaneously changing a total of eight design variables, rather than changing them one at a time as in conventional tradeoff studies. A combination of design variables was in this way identified which yields very attractive vehicle dry and gross weights.

  6. Multi-Response Optimization of Process Parameters for Imidacloprid Removal by Reverse Osmosis Using Taguchi Design.

    PubMed

    Genç, Nevim; Doğan, Esra Can; Narcı, Ali Oğuzhan; Bican, Emine

    2017-05-01

      In this study, a multi-response optimization method using Taguchi's robust design approach is proposed for imidacloprid removal by reverse osmosis. Tests were conducted with different membrane type (BW30, LFC-3, CPA-3), transmembrane pressure (TMP = 20, 25, 30 bar), volume reduction factor (VRF = 2, 3, 4), and pH (3, 7, 11). Quality and quantity of permeate are optimized with the multi-response characteristics of the total dissolved solid (TDS), conductivity, imidacloprid, and total organic carbon (TOC) rejection ratios and flux of permeate. The optimized conditions were determined as membrane type of BW30, TMP 30 bar, VRF 3, and pH 11. Under these conditions, TDS, conductivity, imidacloprid, and TOC rejections and permeate flux were 97.50 97.41, 97.80, 98.00% and 30.60 L/m2·h, respectively. Membrane type was obtained as the most effective factor; its contribution is 64%. The difference between the predicted and observed value of multi-response signal/noise (MRSN) is within the confidence interval.

  7. Application of Taguchi Design and Response Surface Methodology for Improving Conversion of Isoeugenol into Vanillin by Resting Cells of Psychrobacter sp. CSW4.

    PubMed

    Ashengroph, Morahem; Nahvi, Iraj; Amini, Jahanshir

    2013-01-01

    For all industrial processes, modelling, optimisation and control are the keys to enhance productivity and ensure product quality. In the current study, the optimization of process parameters for improving the conversion of isoeugenol to vanillin by Psychrobacter sp. CSW4 was investigated by means of Taguchi approach and Box-Behnken statistical design under resting cell conditions. Taguchi design was employed for screening the significant variables in the bioconversion medium. Sequentially, Box-Behnken design experiments under Response Surface Methodology (RSM) was used for further optimization. Four factors (isoeugenol, NaCl, biomass and tween 80 initial concentrations), which have significant effects on vanillin yield, were selected from ten variables by Taguchi experimental design. With the regression coefficient analysis in the Box-Behnken design, a relationship between vanillin production and four significant variables was obtained, and the optimum levels of the four variables were as follows: initial isoeugenol concentration 6.5 g/L, initial tween 80 concentration 0.89 g/L, initial NaCl concentration 113.2 g/L and initial biomass concentration 6.27 g/L. Under these optimized conditions, the maximum predicted concentration of vanillin was 2.25 g/L. These optimized values of the factors were validated in a triplicate shaking flask study and an average of 2.19 g/L for vanillin, which corresponded to a molar yield 36.3%, after a 24 h bioconversion was obtained. The present work is the first one reporting the application of Taguchi design and Response surface methodology for optimizing bioconversion of isoeugenol into vanillin under resting cell conditions.

  8. Interactive design optimization of magnetorheological-brake actuators using the Taguchi method

    NASA Astrophysics Data System (ADS)

    Erol, Ozan; Gurocak, Hakan

    2011-10-01

    This research explored an optimization method that would automate the process of designing a magnetorheological (MR)-brake but still keep the designer in the loop. MR-brakes apply resistive torque by increasing the viscosity of an MR fluid inside the brake. This electronically controllable brake can provide a very large torque-to-volume ratio, which is very desirable for an actuator. However, the design process is quite complex and time consuming due to many parameters. In this paper, we adapted the popular Taguchi method, widely used in manufacturing, to the problem of designing a complex MR-brake. Unlike other existing methods, this approach can automatically identify the dominant parameters of the design, which reduces the search space and the time it takes to find the best possible design. While automating the search for a solution, it also lets the designer see the dominant parameters and make choices to investigate only their interactions with the design output. The new method was applied for re-designing MR-brakes. It reduced the design time from a week or two down to a few minutes. Also, usability experiments indicated significantly better brake designs by novice users.

  9. Microcosm assays and Taguchi experimental design for treatment of oil sludge containing high concentration of hydrocarbons.

    PubMed

    Castorena-Cortés, G; Roldán-Carrillo, T; Zapata-Peñasco, I; Reyes-Avila, J; Quej-Aké, L; Marín-Cruz, J; Olguín-Lora, P

    2009-12-01

    Microcosm assays and Taguchi experimental design was used to assess the biodegradation of an oil sludge produced by a gas processing unit. The study showed that the biodegradation of the sludge sample is feasible despite the high level of pollutants and complexity involved in the sludge. The physicochemical and microbiological characterization of the sludge revealed a high concentration of hydrocarbons (334,766+/-7001 mg kg(-1) dry matter, d.m.) containing a variety of compounds between 6 and 73 carbon atoms in their structure, whereas the concentration of Fe was 60,000 mg kg(-1) d.m. and 26,800 mg kg(-1) d.m. of sulfide. A Taguchi L(9) experimental design comprising 4 variables and 3 levels moisture, nitrogen source, surfactant concentration and oxidant agent was performed, proving that moisture and nitrogen source are the major variables that affect CO(2) production and total petroleum hydrocarbons (TPH) degradation. The best experimental treatment yielded a TPH removal of 56,092 mg kg(-1) d.m. The treatment was carried out under the following conditions: 70% moisture, no oxidant agent, 0.5% of surfactant and NH(4)Cl as nitrogen source.

  10. Taguchi method for partial differential equations with application in tumor growth.

    PubMed

    Ilea, M; Turnea, M; Rotariu, M; Arotăriţei, D; Popescu, Marilena

    2014-01-01

    The growth of tumors is a highly complex process. To describe this process, mathematical models are needed. A variety of partial differential mathematical models for tumor growth have been developed and studied. Most of those models are based on the reaction-diffusion equations and mass conservation law. A variety of modeling strategies have been developed, each focusing on tumor growth. Systems of time-dependent partial differential equations occur in many branches of applied mathematics. The vast majority of mathematical models in tumor growth are formulated in terms of partial differential equations. We propose a mathematical model for the interactions between these three cancer cell populations. The Taguchi methods are widely used by quality engineering scientists to compare the effects of multiple variables, together with their interactions, with a simple and manageable experimental design. In Taguchi's design of experiments, variation is more interesting to study than the average. First, Taguchi methods are utilized to search for the significant factors and the optimal level combination of parameters. Except the three parameters levels, other factors levels other factors levels would not be considered. Second, cutting parameters namely, cutting speed, depth of cut, and feed rate are designed using the Taguchi method. Finally, the adequacy of the developed mathematical model is proved by ANOVA. According to the results of ANOVA, since the percentage contribution of the combined error is as small. Many mathematical models can be quantitatively characterized by partial differential equations. The use of MATLAB and Taguchi method in this article illustrates the important role of informatics in research in mathematical modeling. The study of tumor growth cells is an exciting and important topic in cancer research and will profit considerably from theoretical input. Interpret these results to be a permanent collaboration between math's and medical oncologists.

  11. Workspace design for crane cabins applying a combined traditional approach and the Taguchi method for design of experiments.

    PubMed

    Spasojević Brkić, Vesna K; Veljković, Zorica A; Golubović, Tamara; Brkić, Aleksandar Dj; Kosić Šotić, Ivana

    2016-01-01

    Procedures in the development process of crane cabins are arbitrary and subjective. Since approximately 42% of incidents in the construction industry are linked to them, there is a need to collect fresh anthropometric data and provide additional recommendations for design. In this paper, dimensioning of the crane cabin interior space was carried out using a sample of 64 crane operators' anthropometric measurements, in the Republic of Serbia, by measuring workspace with 10 parameters using nine measured anthropometric data from each crane operator. This paper applies experiments run via full factorial designs using a combined traditional and Taguchi approach. The experiments indicated which design parameters are influenced by which anthropometric measurements and to what degree. The results are expected to be of use for crane cabin designers and should assist them to design a cabin that may lead to less strenuous sitting postures and fatigue for operators, thus improving safety and accident prevention.

  12. Vertically aligned N-doped CNTs growth using Taguchi experimental design

    NASA Astrophysics Data System (ADS)

    Silva, Ricardo M.; Fernandes, António J. S.; Ferro, Marta C.; Pinna, Nicola; Silva, Rui F.

    2015-07-01

    The Taguchi method with a parameter design L9 orthogonal array was implemented for optimizing the nitrogen incorporation in the structure of vertically aligned N-doped CNTs grown by thermal chemical deposition (TCVD). The maximization of the ID/IG ratio of the Raman spectra was selected as the target value. As a result, the optimal deposition configuration was NH3 = 90 sccm, growth temperature = 825 °C and catalyst pretreatment time of 2 min, the first parameter having the main effect on nitrogen incorporation. A confirmation experiment with these values was performed, ratifying the predicted ID/IG ratio of 1.42. Scanning electron microscopy (SEM) characterization revealed a uniform completely vertically aligned array of multiwalled CNTs which individually exhibit a bamboo-like structure, consisting of periodically curved graphitic layers, as depicted by high resolution transmission electron microscopy (HRTEM). The X-ray photoelectron spectroscopy (XPS) results indicated a 2.00 at.% of N incorporation in the CNTs in pyridine-like and graphite-like, as the predominant species.

  13. Design of Maternity Pillow by Using Kansei and Taguchi Methods

    NASA Astrophysics Data System (ADS)

    Ilma Rahmillah, Fety; Nanda kartika, Rachmah

    2017-06-01

    One of the customers’ considerations for purchasing a product is it can satisfy their feeling and emotion. It because of such product can enhance sleep quality of pregnant women. However, most of the existing product such as maternity pillows are still designed based on companies’ perspective. This study aims to capture the desire of pregnant women toward maternity pillow desired product by using kansei words and analyze the optimal design with Taguchi method. Eight collected kansei words were durable, aesthetic, comfort, portable, simple, multifunction, attractive motive, and easy to maintain. While L16 orthogonal array is used because there are three variables with two levels and four variables with four levels. It can be concluded that the best maternity pillow that can satisfy the customers can be designed by combining D1-E2-F2-G2-C1-B2-A2 means the model is U shape, flowery motive, medium color, Bag model B, cotton pillow cover, filled with silicon, and use double zipper. However, it is also possible to create combination of D1-E2-F2-G2-C1-B1-A1 by using consideration of cost which means that the zipper is switched to single as well as filled with dacron. In addition, the total percentage of contribution by using ANOVA reaches 95%.

  14. Taguchi's off line method and Multivariate loss function approach for quality management and optimization of process parameters -A review

    NASA Astrophysics Data System (ADS)

    Bharti, P. K.; Khan, M. I.; Singh, Harbinder

    2010-10-01

    Off-line quality control is considered to be an effective approach to improve product quality at a relatively low cost. The Taguchi method is one of the conventional approaches for this purpose. Through this approach, engineers can determine a feasible combination of design parameters such that the variability of a product's response can be reduced and the mean is close to the desired target. The traditional Taguchi method was focused on ensuring good performance at the parameter design stage with one quality characteristic, but most products and processes have multiple quality characteristics. The optimal parameter design minimizes the total quality loss for multiple quality characteristics. Several studies have presented approaches addressing multiple quality characteristics. Most of these papers were concerned with maximizing the parameter combination of signal to noise (SN) ratios. The results reveal the advantages of this approach are that the optimal parameter design is the same as the traditional Taguchi method for the single quality characteristic; the optimal design maximizes the amount of reduction of total quality loss for multiple quality characteristics. This paper presents a literature review on solving multi-response problems in the Taguchi method and its successful implementation in various industries.

  15. Application of Taguchi methods to dual mixture ratio propulsion system optimization for SSTO vehicles

    NASA Technical Reports Server (NTRS)

    Stanley, Douglas O.; Unal, Resit; Joyner, C. R.

    1992-01-01

    The application of advanced technologies to future launch vehicle designs would allow the introduction of a rocket-powered, single-stage-to-orbit (SSTO) launch system early in the next century. For a selected SSTO concept, a dual mixture ratio, staged combustion cycle engine that employs a number of innovative technologies was selected as the baseline propulsion system. A series of parametric trade studies are presented to optimize both a dual mixture ratio engine and a single mixture ratio engine of similar design and technology level. The effect of varying lift-off thrust-to-weight ratio, engine mode transition Mach number, mixture ratios, area ratios, and chamber pressure values on overall vehicle weight is examined. The sensitivity of the advanced SSTO vehicle to variations in each of these parameters is presented, taking into account the interaction of each of the parameters with each other. This parametric optimization and sensitivity study employs a Taguchi design method. The Taguchi method is an efficient approach for determining near-optimum design parameters using orthogonal matrices from design of experiments (DOE) theory. Using orthogonal matrices significantly reduces the number of experimental configurations to be studied. The effectiveness and limitations of the Taguchi method for propulsion/vehicle optimization studies as compared to traditional single-variable parametric trade studies is also discussed.

  16. Nitric acid treated multi-walled carbon nanotubes optimized by Taguchi method

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Shamsuddin, Shahidah Arina; Hashim, Uda; Halim, Nur Hamidah Abdul

    Electron transfer rate (ETR) of CNTs can be enhanced by increasing the amounts of COOH groups to their wall and opened tips. With the aim to achieve the highest production amount of COOH, Taguchi robust design has been used for the first time to optimize the surface modification of MWCNTs by nitric acid oxidation. Three main oxidation parameters which are concentration of acid, treatment temperature and treatment time have been selected as the control factors that will be optimized. The amounts of COOH produced are measured by using FTIR spectroscopy through the absorbance intensity. From the analysis, we found thatmore » acid concentration and treatment time had the most important influence on the production of COOH. Meanwhile, the treatment temperature will only give intermediate effect. The optimum amount of COOH can be achieved with the treatment by 8.0 M concentration of nitric acid at 120 °C for 2 hour.« less

  17. Optimization of laccase production from Marasmiellus palmivorus LA1 by Taguchi method of Design of experiments.

    PubMed

    Chenthamarakshan, Aiswarya; Parambayil, Nayana; Miziriya, Nafeesathul; Soumya, P S; Lakshmi, M S Kiran; Ramgopal, Anala; Dileep, Anuja; Nambisan, Padma

    2017-02-13

    Fungal laccase has profound applications in different fields of biotechnology due to its broad specificity and high redox potential. Any successful application of the enzyme requires large scale production. As laccase production is highly dependent on medium components and cultural conditions, optimization of the same is essential for efficient product production. Production of laccase by fungal strain Marasmiellus palmivorus LA1 under solid state fermentation was optimized by the Taguchi design of experiments (DOE) methodology. An orthogonal array (L8) was designed using Qualitek-4 software to study the interactions and relative influence of the seven selected factors by one factor at a time approach. The optimum condition formulated was temperature (28 °C), pH (5), galactose (0.8%w/v), cupric sulphate (3 mM), inoculum concentration (number of mycelial agar pieces) (6Nos.) and substrate length (0.05 m). Overall yield increase of 17.6 fold was obtained after optimization. Statistical optimization leads to the elimination of an insignificant medium component ammonium dihydrogen phosphate from the process and contributes to a 1.06 fold increase in enzyme production. A final production of 667.4 ± 13 IU/mL laccase activity paves way for the application of this strain for industrial applications. Study optimized lignin degrading laccases from Marasmiellus palmivorus LA1. This laccases can thus be used for further applications in different scales of production after analyzing the properties of the enzyme. Study also confirmed the use of taguchi method for optimizations of product production.

  18. Optimization of PID Parameters Utilizing Variable Weight Grey-Taguchi Method and Particle Swarm Optimization

    NASA Astrophysics Data System (ADS)

    Azmi, Nur Iffah Mohamed; Arifin Mat Piah, Kamal; Yusoff, Wan Azhar Wan; Romlay, Fadhlur Rahman Mohd

    2018-03-01

    Controller that uses PID parameters requires a good tuning method in order to improve the control system performance. Tuning PID control method is divided into two namely the classical methods and the methods of artificial intelligence. Particle swarm optimization algorithm (PSO) is one of the artificial intelligence methods. Previously, researchers had integrated PSO algorithms in the PID parameter tuning process. This research aims to improve the PSO-PID tuning algorithms by integrating the tuning process with the Variable Weight Grey- Taguchi Design of Experiment (DOE) method. This is done by conducting the DOE on the two PSO optimizing parameters: the particle velocity limit and the weight distribution factor. Computer simulations and physical experiments were conducted by using the proposed PSO- PID with the Variable Weight Grey-Taguchi DOE and the classical Ziegler-Nichols methods. They are implemented on the hydraulic positioning system. Simulation results show that the proposed PSO-PID with the Variable Weight Grey-Taguchi DOE has reduced the rise time by 48.13% and settling time by 48.57% compared to the Ziegler-Nichols method. Furthermore, the physical experiment results also show that the proposed PSO-PID with the Variable Weight Grey-Taguchi DOE tuning method responds better than Ziegler-Nichols tuning. In conclusion, this research has improved the PSO-PID parameter by applying the PSO-PID algorithm together with the Variable Weight Grey-Taguchi DOE method as a tuning method in the hydraulic positioning system.

  19. Taguchi optimization of bismuth-telluride based thermoelectric cooler

    NASA Astrophysics Data System (ADS)

    Anant Kishore, Ravi; Kumar, Prashant; Sanghadasa, Mohan; Priya, Shashank

    2017-07-01

    In the last few decades, considerable effort has been made to enhance the figure-of-merit (ZT) of thermoelectric (TE) materials. However, the performance of commercial TE devices still remains low due to the fact that the module figure-of-merit not only depends on the material ZT, but also on the operating conditions and configuration of TE modules. This study takes into account comprehensive set of parameters to conduct the numerical performance analysis of the thermoelectric cooler (TEC) using a Taguchi optimization method. The Taguchi method is a statistical tool that predicts the optimal performance with a far less number of experimental runs than the conventional experimental techniques. Taguchi results are also compared with the optimized parameters obtained by a full factorial optimization method, which reveals that the Taguchi method provides optimum or near-optimum TEC configuration using only 25 experiments against 3125 experiments needed by the conventional optimization method. This study also shows that the environmental factors such as ambient temperature and cooling coefficient do not significantly affect the optimum geometry and optimum operating temperature of TECs. The optimum TEC configuration for simultaneous optimization of cooling capacity and coefficient of performance is also provided.

  20. An Exploratory Exercise in Taguchi Analysis of Design Parameters: Application to a Shuttle-to-space Station Automated Approach Control System

    NASA Technical Reports Server (NTRS)

    Deal, Don E.

    1991-01-01

    The chief goals of the summer project have been twofold - first, for my host group and myself to learn as much of the working details of Taguchi analysis as possible in the time allotted, and, secondly, to apply the methodology to a design problem with the intention of establishing a preliminary set of near-optimal (in the sense of producing a desired response) design parameter values from among a large number of candidate factor combinations. The selected problem is concerned with determining design factor settings for an automated approach program which is to have the capability of guiding the Shuttle into the docking port of the Space Station under controlled conditions so as to meet and/or optimize certain target criteria. The candidate design parameters under study were glide path (i.e., approach) angle, path intercept and approach gains, and minimum impulse bit mode (a parameter which defines how Shuttle jets shall be fired). Several performance criteria were of concern: terminal relative velocity at the instant the two spacecraft are mated; docking offset; number of Shuttle jet firings in certain specified directions (of interest due to possible plume impingement on the Station's solar arrays), and total RCS (a measure of the energy expended in performing the approach/docking maneuver). In the material discussed here, we have focused on single performance criteria - total RCS. An analysis of the possibility of employing a multiobjective function composed of a weighted sum of the various individual criteria has been undertaken, but is, at this writing, incomplete. Results from the Taguchi statistical analysis indicate that only three of the original four posited factors are significant in affecting RCS response. A comparison of model simulation output (via Monte Carlo) with predictions based on estimated factor effects inferred through the Taguchi experiment array data suggested acceptable or close agreement between the two except at the predicted optimum

  1. The robust design for improving crude palm oil quality in Indonesian Mill

    NASA Astrophysics Data System (ADS)

    Maretia Benu, Siti; Sinulingga, Sukaria; Matondang, Nazaruddin; Budiman, Irwan

    2018-04-01

    This research was conducted in palm oil mill in Sumatra Utara Province, Indonesia. Currently, the main product of this mill is Crude Palm Oil (CPO) and hasn’t met the expected standard quality. CPO is the raw material for many fat derivative products. The generally stipulated quality criteria are dirt count, free fatty acid, and moisture of CPO. The aim of this study is to obtain the optimal setting for factor’s affect the quality of CPO. The optimal setting will result in an improvement of product’s quality. In this research, Experimental Design with Taguchi Method is used. Steps of this method are identified influence factors, select the orthogonal array, processed data using ANOVA test and signal to noise ratio, and confirmed the research using Quality Loss Function. The result of this study using Taguchi Method is to suggest to set fruit maturity at 75.4-86.9%, digester temperature at 95°C and press at 21 Ampere to reduce quality deviation until 42.42%.

  2. Taguchi-generalized regression neural network micro-screening for physical and sensory characteristics of bread.

    PubMed

    Besseris, George J

    2018-03-01

    Generalized regression neural networks (GRNN) may act as crowdsourcing cognitive agents to screen small, dense and complex datasets. The concurrent screening and optimization of several complex physical and sensory traits of bread is developed using a structured Taguchi-type micro-mining technique. A novel product outlook is offered to industrial operations to cover separate aspects of smart product design, engineering and marketing. Four controlling factors were selected to be modulated directly on a modern production line: 1) the dough weight, 2) the proofing time, 3) the baking time, and 4) the oven zone temperatures. Concentrated experimental recipes were programmed using the Taguchi-type L 9 (3 4 ) OA-sampler to detect potentially non-linear multi-response tendencies. The fused behavior of the master-ranked bread characteristics behavior was smart sampled with GRNN-crowdsourcing and robust analysis. It was found that the combination of the oven zone temperatures to play a highly influential role in all investigated scenarios. Moreover, the oven zone temperatures and the dough weight appeared to be instrumental when attempting to synchronously adjusting all four physical characteristics. The optimal oven-zone temperature setting for concurrent screening-and-optimization was found to be 270-240 °C. The optimized (median) responses for loaf weight, moisture, height, width, color, flavor, crumb structure, softness, and elasticity are: 782 g, 34.8 %, 9.36 cm, 10.41 cm, 6.6, 7.2, 7.6, 7.3, and 7.0, respectively.

  3. Optimization of segmented thermoelectric generator using Taguchi and ANOVA techniques.

    PubMed

    Kishore, Ravi Anant; Sanghadasa, Mohan; Priya, Shashank

    2017-12-01

    Recent studies have demonstrated that segmented thermoelectric generators (TEGs) can operate over large thermal gradient and thus provide better performance (reported efficiency up to 11%) as compared to traditional TEGs, comprising of single thermoelectric (TE) material. However, segmented TEGs are still in early stages of development due to the inherent complexity in their design optimization and manufacturability. In this study, we demonstrate physics based numerical techniques along with Analysis of variance (ANOVA) and Taguchi optimization method for optimizing the performance of segmented TEGs. We have considered comprehensive set of design parameters, such as geometrical dimensions of p-n legs, height of segmentation, hot-side temperature, and load resistance, in order to optimize output power and efficiency of segmented TEGs. Using the state-of-the-art TE material properties and appropriate statistical tools, we provide near-optimum TEG configuration with only 25 experiments as compared to 3125 experiments needed by the conventional optimization methods. The effect of environmental factors on the optimization of segmented TEGs is also studied. Taguchi results are validated against the results obtained using traditional full factorial optimization technique and a TEG configuration for simultaneous optimization of power and efficiency is obtained.

  4. Design optimization for cost and quality: The robust design approach

    NASA Technical Reports Server (NTRS)

    Unal, Resit

    1990-01-01

    Designing reliable, low cost, and operable space systems has become the key to future space operations. Designing high quality space systems at low cost is an economic and technological challenge to the designer. A systematic and efficient way to meet this challenge is a new method of design optimization for performance, quality, and cost, called Robust Design. Robust Design is an approach for design optimization. It consists of: making system performance insensitive to material and subsystem variation, thus allowing the use of less costly materials and components; making designs less sensitive to the variations in the operating environment, thus improving reliability and reducing operating costs; and using a new structured development process so that engineering time is used most productively. The objective in Robust Design is to select the best combination of controllable design parameters so that the system is most robust to uncontrollable noise factors. The robust design methodology uses a mathematical tool called an orthogonal array, from design of experiments theory, to study a large number of decision variables with a significantly small number of experiments. Robust design also uses a statistical measure of performance, called a signal-to-noise ratio, from electrical control theory, to evaluate the level of performance and the effect of noise factors. The purpose is to investigate the Robust Design methodology for improving quality and cost, demonstrate its application by the use of an example, and suggest its use as an integral part of space system design process.

  5. Modified Mahalanobis Taguchi System for Imbalance Data Classification

    PubMed Central

    2017-01-01

    The Mahalanobis Taguchi System (MTS) is considered one of the most promising binary classification algorithms to handle imbalance data. Unfortunately, MTS lacks a method for determining an efficient threshold for the binary classification. In this paper, a nonlinear optimization model is formulated based on minimizing the distance between MTS Receiver Operating Characteristics (ROC) curve and the theoretical optimal point named Modified Mahalanobis Taguchi System (MMTS). To validate the MMTS classification efficacy, it has been benchmarked with Support Vector Machines (SVMs), Naive Bayes (NB), Probabilistic Mahalanobis Taguchi Systems (PTM), Synthetic Minority Oversampling Technique (SMOTE), Adaptive Conformal Transformation (ACT), Kernel Boundary Alignment (KBA), Hidden Naive Bayes (HNB), and other improved Naive Bayes algorithms. MMTS outperforms the benchmarked algorithms especially when the imbalance ratio is greater than 400. A real life case study on manufacturing sector is used to demonstrate the applicability of the proposed model and to compare its performance with Mahalanobis Genetic Algorithm (MGA). PMID:28811820

  6. Application of Taguchi L16 design method for comparative study of ability of 3A zeolite in removal of Rhodamine B and Malachite green from environmental water samples

    NASA Astrophysics Data System (ADS)

    Rahmani, Mashaallah; Kaykhaii, Massoud; Sasani, Mojtaba

    2018-01-01

    This study aimed to investigate the efficiency of 3A zeolite as a novel adsorbent for removal of Rhodamine B and Malachite green dyes from water samples. To increase the removal efficiency, effecting parameters on adsorption process were investigated and optimized by adopting Taguchi design of experiments approach. The percentage contribution of each parameter on the removal of Rhodamine B and Malachite green dyes determined using ANOVA and showed that the most effective parameters in removal of RhB and MG by 3A zeolite are initial concentration of dye and pH, respectively. Under optimized condition, the amount predicted by Taguchi design method and the value obtained experimentally, showed good closeness (more than 94.86%). Good adsorption efficiency obtained for proposed methods indicates that, the 3A zeolite is capable to remove the significant amounts of Rhodamine B and Malachite green from environmental water samples.

  7. Application of Taguchi L16 design method for comparative study of ability of 3A zeolite in removal of Rhodamine B and Malachite green from environmental water samples.

    PubMed

    Rahmani, Mashaallah; Kaykhaii, Massoud; Sasani, Mojtaba

    2018-01-05

    This study aimed to investigate the efficiency of 3A zeolite as a novel adsorbent for removal of Rhodamine B and Malachite green dyes from water samples. To increase the removal efficiency, effecting parameters on adsorption process were investigated and optimized by adopting Taguchi design of experiments approach. The percentage contribution of each parameter on the removal of Rhodamine B and Malachite green dyes determined using ANOVA and showed that the most effective parameters in removal of RhB and MG by 3A zeolite are initial concentration of dye and pH, respectively. Under optimized condition, the amount predicted by Taguchi design method and the value obtained experimentally, showed good closeness (more than 94.86%). Good adsorption efficiency obtained for proposed methods indicates that, the 3A zeolite is capable to remove the significant amounts of Rhodamine B and Malachite green from environmental water samples. Copyright © 2017 Elsevier B.V. All rights reserved.

  8. Optimization of porthole die geometrical variables by Taguchi method

    NASA Astrophysics Data System (ADS)

    Gagliardi, F.; Ciancio, C.; Ambrogio, G.; Filice, L.

    2017-10-01

    Porthole die extrusion is commonly used to manufacture hollow profiles made of lightweight alloys for numerous industrial applications. The reliability of extruded parts is affected strongly by the quality of the longitudinal and transversal seam welds. According to that, the die geometry must be designed correctly and the process parameters must be selected properly to achieve the desired product quality. In this study, numerical 3D simulations have been created and run to investigate the role of various geometrical variables on punch load and maximum pressure inside the welding chamber. These are important outputs to take into account affecting, respectively, the necessary capacity of the extrusion press and the quality of the welding lines. The Taguchi technique has been used to reduce the number of the required numerical simulations necessary for considering the influence of twelve different geometric variables. Moreover, the Analysis of variance (ANOVA) has been implemented to individually analyze the effect of each input parameter on the two responses. Then, the methodology has been utilized to determine the optimal process configuration individually optimizing the two investigated process outputs. Finally, the responses of the optimized parameters have been verified through finite element simulations approximating the predicted value closely. This study shows the feasibility of the Taguchi technique for predicting performance, optimization and therefore for improving the design of a porthole extrusion process.

  9. Robust Crossfeed Design for Hovering Rotorcraft

    NASA Technical Reports Server (NTRS)

    Catapang, David R.

    1993-01-01

    Control law design for rotorcraft fly-by-wire systems normally attempts to decouple angular responses using fixed-gain crossfeeds. This approach can lead to poor decoupling over the frequency range of pilot inputs and increase the load on the feedback loops. In order to improve the decoupling performance, dynamic crossfeeds may be adopted. Moreover, because of the large changes that occur in rotorcraft dynamics due to small changes about the nominal design condition, especially for near-hovering flight, the crossfeed design must be 'robust'. A new low-order matching method is presented here to design robust crossfeed compensators for multi-input, multi-output (MIMO) systems. The technique identifies degrees-of-freedom that can be decoupled using crossfeeds, given an anticipated set of parameter variations for the range of flight conditions of concern. Cross-coupling is then reduced for degrees-of-freedom that can use crossfeed compensation by minimizing off-axis response magnitude average and variance. Results are presented for the analysis of pitch, roll, yaw and heave coupling of the UH-60 Black Hawk helicopter in near-hovering flight. Robust crossfeeds are designed that show significant improvement in decoupling performance and robustness over nominal, single design point, compensators. The design method and results are presented in an easily used graphical format that lends significant physical insight to the design procedure. This plant pre-compensation technique is an appropriate preliminary step to the design of robust feedback control laws for rotorcraft.

  10. Robust design optimization using the price of robustness, robust least squares and regularization methods

    NASA Astrophysics Data System (ADS)

    Bukhari, Hassan J.

    2017-12-01

    In this paper a framework for robust optimization of mechanical design problems and process systems that have parametric uncertainty is presented using three different approaches. Robust optimization problems are formulated so that the optimal solution is robust which means it is minimally sensitive to any perturbations in parameters. The first method uses the price of robustness approach which assumes the uncertain parameters to be symmetric and bounded. The robustness for the design can be controlled by limiting the parameters that can perturb.The second method uses the robust least squares method to determine the optimal parameters when data itself is subjected to perturbations instead of the parameters. The last method manages uncertainty by restricting the perturbation on parameters to improve sensitivity similar to Tikhonov regularization. The methods are implemented on two sets of problems; one linear and the other non-linear. This methodology will be compared with a prior method using multiple Monte Carlo simulation runs which shows that the approach being presented in this paper results in better performance.

  11. Robustness Analysis and Optimally Robust Control Design via Sum-of-Squares

    NASA Technical Reports Server (NTRS)

    Dorobantu, Andrei; Crespo, Luis G.; Seiler, Peter J.

    2012-01-01

    A control analysis and design framework is proposed for systems subject to parametric uncertainty. The underlying strategies are based on sum-of-squares (SOS) polynomial analysis and nonlinear optimization to design an optimally robust controller. The approach determines a maximum uncertainty range for which the closed-loop system satisfies a set of stability and performance requirements. These requirements, de ned as inequality constraints on several metrics, are restricted to polynomial functions of the uncertainty. To quantify robustness, SOS analysis is used to prove that the closed-loop system complies with the requirements for a given uncertainty range. The maximum uncertainty range, calculated by assessing a sequence of increasingly larger ranges, serves as a robustness metric for the closed-loop system. To optimize the control design, nonlinear optimization is used to enlarge the maximum uncertainty range by tuning the controller gains. Hence, the resulting controller is optimally robust to parametric uncertainty. This approach balances the robustness margins corresponding to each requirement in order to maximize the aggregate system robustness. The proposed framework is applied to a simple linear short-period aircraft model with uncertain aerodynamic coefficients.

  12. Near Field and Far Field Effects in the Taguchi-Optimized Design of AN InP/GaAs-BASED Double Wafer-Fused Mqw Long-Wavelength Vertical-Cavity Surface-Emitting Laser

    NASA Astrophysics Data System (ADS)

    Menon, P. S.; Kandiah, K.; Mandeep, J. S.; Shaari, S.; Apte, P. R.

    Long-wavelength VCSELs (LW-VCSEL) operating in the 1.55 μm wavelength regime offer the advantages of low dispersion and optical loss in fiber optic transmission systems which are crucial in increasing data transmission speed and reducing implementation cost of fiber-to-the-home (FTTH) access networks. LW-VCSELs are attractive light sources because they offer unique features such as low power consumption, narrow beam divergence and ease of fabrication for two-dimensional arrays. This paper compares the near field and far field effects of the numerically investigated LW-VCSEL for various design parameters of the device. The optical intensity profile far from the device surface, in the Fraunhofer region, is important for the optical coupling of the laser with other optical components. The near field pattern is obtained from the structure output whereas the far-field pattern is essentially a two-dimensional fast Fourier Transform (FFT) of the near-field pattern. Design parameters such as the number of wells in the multi-quantum-well (MQW) region, the thickness of the MQW and the effect of using Taguchi's orthogonal array method to optimize the device design parameters on the near/far field patterns are evaluated in this paper. We have successfully increased the peak lasing power from an initial 4.84 mW to 12.38 mW at a bias voltage of 2 V and optical wavelength of 1.55 μm using Taguchi's orthogonal array. As a result of the Taguchi optimization and fine tuning, the device threshold current is found to increase along with a slight decrease in the modulation speed due to increased device widths.

  13. Engineering Design Education Program for Graduate School

    NASA Astrophysics Data System (ADS)

    Ohbuchi, Yoshifumi; Iida, Haruhiko

    The new educational methods of engineering design have attempted to improve mechanical engineering education for graduate students in a way of the collaboration in education of engineer and designer. The education program is based on the lecture and practical exercises concerning the product design, and has engineering themes and design process themes, i.e. project management, QFD, TRIZ, robust design (Taguchi method) , ergonomics, usability, marketing, conception etc. At final exercise, all students were able to design new product related to their own research theme by applying learned knowledge and techniques. By the method of engineering design education, we have confirmed that graduate students are able to experience technological and creative interest.

  14. Designing robust control laws using genetic algorithms

    NASA Technical Reports Server (NTRS)

    Marrison, Chris

    1994-01-01

    The purpose of this research is to create a method of finding practical, robust control laws. The robustness of a controller is judged by Stochastic Robustness metrics and the level of robustness is optimized by searching for design parameters that minimize a robustness cost function.

  15. Application of Taguchi optimisation of electro metal - electro winning (EMEW) for nickel metal from laterite

    NASA Astrophysics Data System (ADS)

    Sudibyo, Hermida, L.; Junaedi, A.; Putra, F. A.

    2017-11-01

    Nickel and cobalt metal able to process from low grade laterite using solvent extraction and electrowinning. One of electrowinning methods which has good performance to produce pure metal is electrometal-electrowinninge(EMEW). In this work, solventextraction was used to separate nickel and cobalt which useCyanex-Versatic Acid in toluene as an organic phase. An aqueous phase of extraction was processed using EMEW in order to deposit the nickel metal in Cathode electrode. The parameters which used in this work were batch temperature, operation time, voltage, and boric acid concentration. Those parameters were studied and optimized using the design of experiment of Taguchi. The Taguchi analysis result shows that the optimum result of EMEW was at 60°C of batch temperature, 2 Voltage, 6 hours operation and 0.5 M of boric acid.

  16. Using Design Capability Indices to Satisfy Ranged Sets of Design Requirements

    NASA Technical Reports Server (NTRS)

    Chen, Wei; Allen, Janet K.; Simpson, Timothy W.; Mistree, Farrokh

    1996-01-01

    For robust design it is desirable to allow the design requirements to vary within a certain range rather than setting point targets. This is particularly important during the early stages of design when little is known about the system and its requirements. Toward this end, design capability indices are developed in this paper to assess the capability of a family of designs, represented by a range of top-level design specifications, to satisfy a ranged set of design requirements. Design capability indices are based on process capability indices from statistical process control and provide a single objective, alternate approach to the use of Taguchi's signal-to- noise ratio which is often used for robust design. Successful implementation of design capability indices ensures that a family of designs conforms to a given ranged set of design requirements. To demonstrate an application and the usefulness of design capability indices, the design of a solar powered irrigation system is presented. Our focus in this paper is on the development and implementation of design capability indices as an alternate approach to the use of the signal-to-noise ratio and not on the results of the example problem, per se.

  17. The Problem of Size in Robust Design

    NASA Technical Reports Server (NTRS)

    Koch, Patrick N.; Allen, Janet K.; Mistree, Farrokh; Mavris, Dimitri

    1997-01-01

    To facilitate the effective solution of multidisciplinary, multiobjective complex design problems, a departure from the traditional parametric design analysis and single objective optimization approaches is necessary in the preliminary stages of design. A necessary tradeoff becomes one of efficiency vs. accuracy as approximate models are sought to allow fast analysis and effective exploration of a preliminary design space. In this paper we apply a general robust design approach for efficient and comprehensive preliminary design to a large complex system: a high speed civil transport (HSCT) aircraft. Specifically, we investigate the HSCT wing configuration design, incorporating life cycle economic uncertainties to identify economically robust solutions. The approach is built on the foundation of statistical experimentation and modeling techniques and robust design principles, and is specialized through incorporation of the compromise Decision Support Problem for multiobjective design. For large problems however, as in the HSCT example, this robust design approach developed for efficient and comprehensive design breaks down with the problem of size - combinatorial explosion in experimentation and model building with number of variables -and both efficiency and accuracy are sacrificed. Our focus in this paper is on identifying and discussing the implications and open issues associated with the problem of size for the preliminary design of large complex systems.

  18. Bioremediation of chlorpyrifos contaminated soil by two phase bioslurry reactor: Processes evaluation and optimization by Taguchi's design of experimental (DOE) methodology.

    PubMed

    Pant, Apourv; Rai, J P N

    2018-04-15

    Two phase bioreactor was constructed, designed and developed to evaluate the chlorpyrifos remediation. Six biotic and abiotic factors (substrate-loading rate, slurry phase pH, slurry phase dissolved oxygen (DO), soil water ratio, temperature and soil micro flora load) were evaluated by design of experimental (DOE) methodology employing Taguchi's orthogonal array (OA). The selected six factors were considered at two levels L-8 array (2^7, 15 experiments) in the experimental design. The optimum operating conditions obtained from the methodology showed enhanced chlorpyrifos degradation from 283.86µg/g to 955.364µg/g by overall 70.34% of enhancement. In the present study, with the help of few well defined experimental parameters a mathematical model was constructed to understand the complex bioremediation process and optimize the approximate parameters upto great accuracy. Copyright © 2017 Elsevier Inc. All rights reserved.

  19. A pre-operative planning for endoprosthetic human tracheal implantation: a decision support system based on robust design of experiments.

    PubMed

    Trabelsi, O; Villalobos, J L López; Ginel, A; Cortes, E Barrot; Doblaré, M

    2014-05-01

    Swallowing depends on physiological variables that have a decisive influence on the swallowing capacity and on the tracheal stress distribution. Prosthetic implantation modifies these values and the overall performance of the trachea. The objective of this work was to develop a decision support system based on experimental, numerical and statistical approaches, with clinical verification, to help the thoracic surgeon in deciding the position and appropriate dimensions of a Dumon prosthesis for a specific patient in an optimal time and with sufficient robustness. A code for mesh adaptation to any tracheal geometry was implemented and used to develop a robust experimental design, based on the Taguchi's method and the analysis of variance. This design was able to establish the main swallowing influencing factors. The equations to fit the stress and the vertical displacement distributions were obtained. The resulting fitted values were compared to those calculated directly by the finite element method (FEM). Finally, a checking and clinical validation of the statistical study were made, by studying two cases of real patients. The vertical displacements and principal stress distribution obtained for the specific tracheal model were in agreement with those calculated by FE simulations with a maximum absolute error of 1.2 mm and 0.17 MPa, respectively. It was concluded that the resulting decision support tool provides a fast, accurate and simple tool for the thoracic surgeon to predict the stress state of the trachea and the reduction in the ability to swallow after implantation. Thus, it will help them in taking decisions during pre-operative planning of tracheal interventions.

  20. Evaluation of B. subtilis SPB1 biosurfactants' potency for diesel-contaminated soil washing: optimization of oil desorption using Taguchi design.

    PubMed

    Mnif, Inès; Sahnoun, Rihab; Ellouze-Chaabouni, Semia; Ghribi, Dhouha

    2014-01-01

    Low solubility of certain hydrophobic soil contaminants limits remediation process. Surface-active compounds can improve the solubility and removal of hydrophobic compounds from contaminated soils and, consequently, their biodegradation. Hence, this paper aims to study desorption efficiency of oil from soil of SPB1 lipopeptide biosurfactant. The effect of different physicochemical parameters on desorption potency was assessed. Taguchi experimental design method was applied in order to enhance the desorption capacity and establish the best washing parameters. Mobilization potency was compared to those of chemical surfactants under the newly defined conditions. Better desorption capacity was obtained using 0.1% biosurfacatnt solution and the mobilization potency shows great tolerance to acidic and alkaline pH values and salinity. Results show an optimum value of oil removal from diesel-contaminated soil of about 87%. The optimum washing conditions for surfactant solution volume, biosurfactant concentration, agitation speed, temperature, and time were found to be 12 ml/g of soil, 0.1% biosurfactant, 200 rpm, 30 °C, and 24 h, respectively. The obtained results were compared to those of SDS and Tween 80 at the optimal conditions described above, and the study reveals an effectiveness of SPB1 biosurfactant comparable to the reported chemical emulsifiers. (1) The obtained findings suggest (a) the competence of Bacillus subtilis biosurfactant in promoting diesel desorption from soil towards chemical surfactants and (b) the applicability of this method in decontaminating crude oil-contaminated soil and, therefore, improving bioavailability of hydrophobic compounds. (2) The obtained findings also suggest the adequacy of Taguchi design in promoting process efficiency. Our findings suggest that preoptimized desorption process using microbial-derived emulsifier can contribute significantly to enhancement of hydrophobic pollutants' bioavailability. This study can be

  1. Nickel-Cadmium Battery Operation Management Optimization Using Robust Design

    NASA Technical Reports Server (NTRS)

    Blosiu, Julian O.; Deligiannis, Frank; DiStefano, Salvador

    1996-01-01

    In recent years following several spacecraft battery anomalies, it was determined that managing the operational factors of NASA flight NiCd rechargeable battery was very important in order to maintain space flight battery nominal performance. The optimization of existing flight battery operational performance was viewed as something new for a Taguchi Methods application.

  2. The parameters effect on the structural performance of damaged steel box beam using Taguchi method

    NASA Astrophysics Data System (ADS)

    El-taly, Boshra A.; Abd El Hameed, Mohamed F.

    2018-03-01

    In the current study, the influence of notch or opening parameters and the positions of the applied load on the structural performance of steel box beams up to failure was investigated using Finite Element analysis program, ANSYS. The Taguchi-based design of experiments technique was used to plan the current study. The plan included 12 box steel beams; three intact beams, and nine damaged beams (with opening) in the beams web. The numerical studies were conducted under varying the spacing between the two concentrated point loads (location of applied loads), the notch (opening) position, and the ratio between depth and width of the notch with a constant notch area. According to Taguchi analysis, factor X (location of the applied loads) was found the highest contributing parameters for the variation of the ultimate load, vertical deformation, shear stresses, and the compressive normal stresses.

  3. Investigation of Structures of Microwave Microelectromechanical-System Switches by Taguchi Method

    NASA Astrophysics Data System (ADS)

    Lai, Yeong-Lin; Lin, Chien-Hung

    2007-10-01

    The optimal design of microwave microelectromechanical-system (MEMS) switches by the Taguchi method is presented. The structures of the switches are analyzed and optimized in terms of the effective stiffness constant, the maximum von Mises stress, and the natural frequency in order to improve the reliability and the performance of the MEMS switches. There are four factors, each of which has three levels in the Taguchi method for the MEMS switches. An L9(34) orthogonal array is used for the matrix experiments. The characteristics of the experiments are studied by the finite-element method and the analytical method. The responses of the signal-to-noise (S/N) ratios of the characteristics of the switches are investigated. The statistical analysis of variance (ANOVA) is used to interpret the experimental results and decide the significant factors. The final optimum setting, A1B3C1D2, predicts that the effective stiffness constant is 1.06 N/m, the maximum von Mises stress is 76.9 MPa, and the natural frequency is 29.331 kHz. The corresponding switching time is 34 μs, and the pull-down voltage is 9.8 V.

  4. Taguchi's technique: an effective method for improving X-ray medical radiographic screen performance.

    PubMed

    Vlachogiannis, J G

    2003-01-01

    Taguchi's technique is a helpful tool to achieve experimental optimization of a large number of decision variables with a small number of off-line experiments. The technique appears to be an ideal tool for improving the performance of X-ray medical radiographic screens under a noise source. Currently there are very many guides available for improving the efficiency of X-ray medical radiographic screens. These guides can be refined using a second-stage parameter optimization. based on Taguchi's technique, selecting the optimum levels of controllable X-ray radiographic screen factors. A real example of the proposed technique is presented giving certain performance criteria. The present research proposes the reinforcement of X-ray radiography by Taguchi's technique as a novel hardware mechanism.

  5. Robust input design for nonlinear dynamic modeling of AUV.

    PubMed

    Nouri, Nowrouz Mohammad; Valadi, Mehrdad

    2017-09-01

    Input design has a dominant role in developing the dynamic model of autonomous underwater vehicles (AUVs) through system identification. Optimal input design is the process of generating informative inputs that can be used to generate the good quality dynamic model of AUVs. In a problem with optimal input design, the desired input signal depends on the unknown system which is intended to be identified. In this paper, the input design approach which is robust to uncertainties in model parameters is used. The Bayesian robust design strategy is applied to design input signals for dynamic modeling of AUVs. The employed approach can design multiple inputs and apply constraints on an AUV system's inputs and outputs. Particle swarm optimization (PSO) is employed to solve the constraint robust optimization problem. The presented algorithm is used for designing the input signals for an AUV, and the estimate obtained by robust input design is compared with that of the optimal input design. According to the results, proposed input design can satisfy both robustness of constraints and optimality. Copyright © 2017 ISA. Published by Elsevier Ltd. All rights reserved.

  6. A Comparative Analysis of Taguchi Methodology and Shainin System DoE in the Optimization of Injection Molding Process Parameters

    NASA Astrophysics Data System (ADS)

    Khavekar, Rajendra; Vasudevan, Hari, Dr.; Modi, Bhavik

    2017-08-01

    Two well-known Design of Experiments (DoE) methodologies, such as Taguchi Methods (TM) and Shainin Systems (SS) are compared and analyzed in this study through their implementation in a plastic injection molding unit. Experiments were performed at a perfume bottle cap manufacturing company (made by acrylic material) using TM and SS to find out the root cause of defects and to optimize the process parameters for minimum rejection. Experiments obtained the rejection rate to be 8.57% from 40% (appx.) during trial runs, which is quiet low, representing successful implementation of these DoE methods. The comparison showed that both methodologies gave same set of variables as critical for defect reduction, but with change in their significance order. Also, Taguchi methods require more number of experiments and consume more time compared to the Shainin System. Shainin system is less complicated and is easy to implement, whereas Taguchi methods is statistically more reliable for optimization of process parameters. Finally, experimentations implied that DoE methods are strong and reliable in implementation, as organizations attempt to improve the quality through optimization.

  7. Use of Taguchi methodology to enhance the yield of caffeine removal with growing cultures of Pseudomonas pseudoalcaligenes.

    PubMed

    Ashengroph, Morahem; Ababaf, Sajad

    2014-12-01

    Microbial caffeine removal is a green solution for treatment of caffeinated products and agro-industrial effluents. We directed this investigation to optimizing a bio-decaffeination process with growing cultures of Pseudomonas pseudoalcaligenes through Taguchi methodology which is a structured statistical approach that can be lowered variations in a process through Design of Experiments (DOE). Five parameters, i.e. initial fructose, tryptone, Zn(+2) ion and caffeine concentrations and also incubation time selected and an L16 orthogonal array was applied to design experiments with four 4-level factors and one 3-level factor (4(4) × 1(3)). Data analysis was performed using the statistical analysis of variance (ANOVA) method. Furthermore, the optimal conditions were determined by combining the optimal levels of the significant factors and verified by a confirming experiment. Measurement of residual caffeine concentration in the reaction mixture was performed using high-performance liquid chromatography (HPLC). Use of Taguchi methodology for optimization of design parameters resulted in about 86.14% reduction of caffeine in 48 h incubation when 5g/l fructose, 3 mM Zn(+2) ion and 4.5 g/l of caffeine are present in the designed media. Under the optimized conditions, the yield of degradation of caffeine (4.5 g/l) by the native strain of Pseudomonas pseudoalcaligenes TPS8 has been increased from 15.8% to 86.14% which is 5.4 fold higher than the normal yield. According to the experimental results, Taguchi methodology provides a powerful methodology for identifying the favorable parameters on caffeine removal using strain TPS8 which suggests that the approach also has potential application with similar strains to improve the yield of caffeine removal from caffeine containing solutions.

  8. Design principles for robust oscillatory behavior.

    PubMed

    Castillo-Hair, Sebastian M; Villota, Elizabeth R; Coronado, Alberto M

    2015-09-01

    Oscillatory responses are ubiquitous in regulatory networks of living organisms, a fact that has led to extensive efforts to study and replicate the circuits involved. However, to date, design principles that underlie the robustness of natural oscillators are not completely known. Here we study a three-component enzymatic network model in order to determine the topological requirements for robust oscillation. First, by simulating every possible topological arrangement and varying their parameter values, we demonstrate that robust oscillators can be obtained by augmenting the number of both negative feedback loops and positive autoregulations while maintaining an appropriate balance of positive and negative interactions. We then identify network motifs, whose presence in more complex topologies is a necessary condition for obtaining oscillatory responses. Finally, we pinpoint a series of simple architectural patterns that progressively render more robust oscillators. Together, these findings can help in the design of more reliable synthetic biomolecular networks and may also have implications in the understanding of other oscillatory systems.

  9. Robust synthetic biology design: stochastic game theory approach.

    PubMed

    Chen, Bor-Sen; Chang, Chia-Hung; Lee, Hsiao-Ching

    2009-07-15

    Synthetic biology is to engineer artificial biological systems to investigate natural biological phenomena and for a variety of applications. However, the development of synthetic gene networks is still difficult and most newly created gene networks are non-functioning due to uncertain initial conditions and disturbances of extra-cellular environments on the host cell. At present, how to design a robust synthetic gene network to work properly under these uncertain factors is the most important topic of synthetic biology. A robust regulation design is proposed for a stochastic synthetic gene network to achieve the prescribed steady states under these uncertain factors from the minimax regulation perspective. This minimax regulation design problem can be transformed to an equivalent stochastic game problem. Since it is not easy to solve the robust regulation design problem of synthetic gene networks by non-linear stochastic game method directly, the Takagi-Sugeno (T-S) fuzzy model is proposed to approximate the non-linear synthetic gene network via the linear matrix inequality (LMI) technique through the Robust Control Toolbox in Matlab. Finally, an in silico example is given to illustrate the design procedure and to confirm the efficiency and efficacy of the proposed robust gene design method. http://www.ee.nthu.edu.tw/bschen/SyntheticBioDesign_supplement.pdf.

  10. Design for robustness of unique, multi-component engineering systems

    NASA Astrophysics Data System (ADS)

    Shelton, Kenneth A.

    2007-12-01

    The purpose of this research is to advance the science of conceptual designing for robustness in unique, multi-component engineering systems. Robustness is herein defined as the ability of an engineering system to operate within a desired performance range even if the actual configuration has differences from specifications within specified tolerances. These differences are caused by three sources, namely manufacturing errors, system degradation (operational wear and tear), and parts availability. Unique, multi-component engineering systems are defined as systems produced in unique or very small production numbers. They typically have design and manufacturing costs on the order of billions of dollars, and have multiple, competing performance objectives. Design time for these systems must be minimized due to competition, high manpower costs, long manufacturing times, technology obsolescence, and limited available manpower expertise. Most importantly, design mistakes cannot be easily corrected after the systems are operational. For all these reasons, robustness of these systems is absolutely critical. This research examines the space satellite industry in particular. Although inherent robustness assurance is absolutely critical, it is difficult to achieve in practice. The current state of the art for robustness in the industry is to overdesign components and subsystems with redundancy and margin. The shortfall is that it is not known if the added margins were either necessary or sufficient given the risk management preferences of the designer or engineering system customer. To address this shortcoming, new assessment criteria to evaluate robustness in design concepts have been developed. The criteria are comprised of the "Value Distance", addressing manufacturing errors and system degradation, and "Component Distance", addressing parts availability. They are based on an evolutionary computation format that uses a string of alleles to describe the components in the

  11. Oily wastewater treatment by ultrafiltration using Taguchi experimental design.

    PubMed

    Salahi, A; Mohammadi, T

    2011-01-01

    In this research, results of an experimental investigation on separation of oil from a real oily wastewater using an ultrafiltration (UF) polymeric membrane are presented. In order to enhance the performance of UF in API separator effluent treatment and to get more permeation flux (PF), effects of operating factors on the yield of PF were studied. Five factors at four levels were investigated: trans-membrane pressure (TMP), temperature (T), cross flow velocity (CFV), pH and salt concentration (SC). Taguchi method (L(16) orthogonal array (OA)) was used. Analysis of variance (ANOVA) was applied to calculate sum of square, variance, error variance and contribution percentage of each factor on response. The optimal levels thus determined for the four influential factors were: TMP, 3 bar; T, 40˚C; CFV, 1.0 m/s; SC, 25 g/L and pH, 8. The results showed that CFV and SC are the most and the least effective factors on PF, respectively. Increasing CFV, TMP, T and pH caused the better performance of UF membrane process due to enhancement of driving force and fouling residence. Also, effects of oil concentration (OC) in the wastewater on PF and total organic carbon (TOC) rejection were investigated. Finally, the highest TOC rejection was found to be 85%.

  12. A minimum cost tolerance allocation method for rocket engines and robust rocket engine design

    NASA Technical Reports Server (NTRS)

    Gerth, Richard J.

    1993-01-01

    Rocket engine design follows three phases: systems design, parameter design, and tolerance design. Systems design and parameter design are most effectively conducted in a concurrent engineering (CE) environment that utilize methods such as Quality Function Deployment and Taguchi methods. However, tolerance allocation remains an art driven by experience, handbooks, and rules of thumb. It was desirable to develop and optimization approach to tolerancing. The case study engine was the STME gas generator cycle. The design of the major components had been completed and the functional relationship between the component tolerances and system performance had been computed using the Generic Power Balance model. The system performance nominals (thrust, MR, and Isp) and tolerances were already specified, as were an initial set of component tolerances. However, the question was whether there existed an optimal combination of tolerances that would result in the minimum cost without any degradation in system performance.

  13. Evaluation of Listeria monocytogenes survival in ice cream mixes flavored with herbal tea using Taguchi method.

    PubMed

    Ozturk, Ismet; Golec, Adem; Karaman, Safa; Sagdic, Osman; Kayacier, Ahmed

    2010-10-01

    In this study, the effects of the incorporation of some herbal teas at different concentrations into the ice cream mix on the population of Listeria monocytogenes were studied using Taguchi method. The ice cream mix samples flavored with herbal teas were prepared using green tea and sage at different concentrations. Afterward, fresh culture of L. monocytogenes was inoculated into the samples and the L. monocytogenes was counted at different storage periods. Taguchi method was used for experimental design and analysis. In addition, some physicochemical properties of samples were examined. Results suggested that there was some effect, although little, on the population of L. monocytogenes when herbal tea was incorporated into the ice cream mix. Additionally, the use of herbal tea caused a decrease in the pH values of the samples and significant changes in the color values.

  14. Designing Phononic Crystals with Wide and Robust Band Gaps

    NASA Astrophysics Data System (ADS)

    Jia, Zian; Chen, Yanyu; Yang, Haoxiang; Wang, Lifeng

    2018-04-01

    Phononic crystals (PnCs) engineered to manipulate and control the propagation of mechanical waves have enabled the design of a range of novel devices, such as waveguides, frequency modulators, and acoustic cloaks, for which wide and robust phononic band gaps are highly preferable. While numerous PnCs have been designed in recent decades, to the best of our knowledge, PnCs that possess simultaneous wide and robust band gaps (to randomness and deformations) have not yet been reported. Here, we demonstrate that by combining the band-gap formation mechanisms of Bragg scattering and local resonances (the latter one is dominating), PnCs with wide and robust phononic band gaps can be established. The robustness of the phononic band gaps are then discussed from two aspects: robustness to geometric randomness (manufacture defects) and robustness to deformations (mechanical stimuli). Analytical formulations further predict the optimal design parameters, and an uncertainty analysis quantifies the randomness effect of each designing parameter. Moreover, we show that the deformation robustness originates from a local resonance-dominant mechanism together with the suppression of structural instability. Importantly, the proposed PnCs require only a small number of layers of elements (three unit cells) to obtain broad, robust, and strong attenuation bands, which offer great potential in designing flexible and deformable phononic devices.

  15. Thermal design, rating and second law analysis of shell and tube condensers based on Taguchi optimization for waste heat recovery based thermal desalination plants

    NASA Astrophysics Data System (ADS)

    Chandrakanth, Balaji; Venkatesan, G; Prakash Kumar, L. S. S; Jalihal, Purnima; Iniyan, S

    2018-03-01

    The present work discusses the design and selection of a shell and tube condenser used in Low Temperature Thermal Desalination (LTTD). To optimize the key geometrical and process parameters of the condenser with multiple parameters and levels, a design of an experiment approach using Taguchi method was chosen. An orthogonal array (OA) of 25 designs was selected for this study. The condenser was designed, analysed using HTRI software and the heat transfer area with respective tube side pressure drop were computed using the same, as these two objective functions determine the capital and running cost of the condenser. There was a complex trade off between the heat transfer area and pressure drop in the analysis, however second law analysis was worked out for determining the optimal heat transfer area vs pressure drop for condensing the required heat load.

  16. Robustness-Based Design Optimization Under Data Uncertainty

    NASA Technical Reports Server (NTRS)

    Zaman, Kais; McDonald, Mark; Mahadevan, Sankaran; Green, Lawrence

    2010-01-01

    This paper proposes formulations and algorithms for design optimization under both aleatory (i.e., natural or physical variability) and epistemic uncertainty (i.e., imprecise probabilistic information), from the perspective of system robustness. The proposed formulations deal with epistemic uncertainty arising from both sparse and interval data without any assumption about the probability distributions of the random variables. A decoupled approach is proposed in this paper to un-nest the robustness-based design from the analysis of non-design epistemic variables to achieve computational efficiency. The proposed methods are illustrated for the upper stage design problem of a two-stage-to-orbit (TSTO) vehicle, where the information on the random design inputs are only available as sparse point and/or interval data. As collecting more data reduces uncertainty but increases cost, the effect of sample size on the optimality and robustness of the solution is also studied. A method is developed to determine the optimal sample size for sparse point data that leads to the solutions of the design problem that are least sensitive to variations in the input random variables.

  17. Designing Phononic Crystals with Wide and Robust Band Gaps

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Jia, Zian; Chen, Yanyu; Yang, Haoxiang

    Here, phononic crystals (PnCs) engineered to manipulate and control the propagation of mechanical waves have enabled the design of a range of novel devices, such as waveguides, frequency modulators, and acoustic cloaks, for which wide and robust phononic band gaps are highly preferable. While numerous PnCs have been designed in recent decades, to the best of our knowledge, PnCs that possess simultaneous wide and robust band gaps (to randomness and deformations) have not yet been reported. Here, we demonstrate that by combining the band-gap formation mechanisms of Bragg scattering and local resonances (the latter one is dominating), PnCs with widemore » and robust phononic band gaps can be established. The robustness of the phononic band gaps are then discussed from two aspects: robustness to geometric randomness (manufacture defects) and robustness to deformations (mechanical stimuli). Analytical formulations further predict the optimal design parameters, and an uncertainty analysis quantifies the randomness effect of each designing parameter. Moreover, we show that the deformation robustness originates from a local resonance-dominant mechanism together with the suppression of structural instability. Importantly, the proposed PnCs require only a small number of layers of elements (three unit cells) to obtain broad, robust, and strong attenuation bands, which offer great potential in designing flexible and deformable phononic devices.« less

  18. Designing Phononic Crystals with Wide and Robust Band Gaps

    DOE PAGES

    Jia, Zian; Chen, Yanyu; Yang, Haoxiang; ...

    2018-04-16

    Here, phononic crystals (PnCs) engineered to manipulate and control the propagation of mechanical waves have enabled the design of a range of novel devices, such as waveguides, frequency modulators, and acoustic cloaks, for which wide and robust phononic band gaps are highly preferable. While numerous PnCs have been designed in recent decades, to the best of our knowledge, PnCs that possess simultaneous wide and robust band gaps (to randomness and deformations) have not yet been reported. Here, we demonstrate that by combining the band-gap formation mechanisms of Bragg scattering and local resonances (the latter one is dominating), PnCs with widemore » and robust phononic band gaps can be established. The robustness of the phononic band gaps are then discussed from two aspects: robustness to geometric randomness (manufacture defects) and robustness to deformations (mechanical stimuli). Analytical formulations further predict the optimal design parameters, and an uncertainty analysis quantifies the randomness effect of each designing parameter. Moreover, we show that the deformation robustness originates from a local resonance-dominant mechanism together with the suppression of structural instability. Importantly, the proposed PnCs require only a small number of layers of elements (three unit cells) to obtain broad, robust, and strong attenuation bands, which offer great potential in designing flexible and deformable phononic devices.« less

  19. Trading Robustness Requirements in Mars Entry Trajectory Design

    NASA Technical Reports Server (NTRS)

    Lafleur, Jarret M.

    2009-01-01

    One of the most important metrics characterizing an atmospheric entry trajectory in preliminary design is the size of its predicted landing ellipse. Often, requirements for this ellipse are set early in design and significantly influence both the expected scientific return from a particular mission and the cost of development. Requirements typically specify a certain probability level (6-level) for the prescribed ellipse, and frequently this latter requirement is taken at 36. However, searches for the justification of 36 as a robustness requirement suggest it is an empirical rule of thumb borrowed from non-aerospace fields. This paper presents an investigation into the sensitivity of trajectory performance to varying robustness (6-level) requirements. The treatment of robustness as a distinct objective is discussed, and an analysis framework is presented involving the manipulation of design variables to effect trades between performance and robustness objectives. The scenario for which this method is illustrated is the ballistic entry of an MSL-class Mars entry vehicle. Here, the design variable is entry flight path angle, and objectives are parachute deploy altitude performance and error ellipse robustness. Resulting plots show the sensitivities between these objectives and trends in the entry flight path angles required to design to these objectives. Relevance to the trajectory designer is discussed, as are potential steps for further development and use of this type of analysis.

  20. Taguchi Optimization of Pulsed Current GTA Welding Parameters for Improved Corrosion Resistance of 5083 Aluminum Welds

    NASA Astrophysics Data System (ADS)

    Rastkerdar, E.; Shamanian, M.; Saatchi, A.

    2013-04-01

    In this study, the Taguchi method was used as a design of experiment (DOE) technique to optimize the pulsed current gas tungsten arc welding (GTAW) parameters for improved pitting corrosion resistance of AA5083-H18 aluminum alloy welds. A L9 (34) orthogonal array of the Taguchi design was used, which involves nine experiments for four parameters: peak current ( P), base current ( B), percent pulse-on time ( T), and pulse frequency ( F) with three levels was used. Pitting corrosion resistance in 3.5 wt.% NaCl solution was evaluated by anodic polarization tests at room temperature and calculating the width of the passive region (∆ E pit). Analysis of variance (ANOVA) was performed on the measured data and S/ N (signal to noise) ratios. The "bigger is better" was selected as the quality characteristic (QC). The optimum conditions were found as 170 A, 85 A, 40%, and 6 Hz for P, B, T, and F factors, respectively. The study showed that the percent pulse-on time has the highest influence on the pitting corrosion resistance (50.48%) followed by pulse frequency (28.62%), peak current (11.05%) and base current (9.86%). The range of optimum ∆ E pit at optimum conditions with a confidence level of 90% was predicted to be between 174.81 and 177.74 mVSCE. Under optimum conditions, the confirmation test was carried out, and the experimental value of ∆ E pit of 176 mVSCE was in agreement with the predicted value from the Taguchi model. In this regard, the model can be effectively used to predict the ∆ E pit of pulsed current gas tungsten arc welded joints.

  1. Application of Taguchi approach to optimize the sol-gel process of the quaternary Cu2ZnSnS4 with good optical properties

    NASA Astrophysics Data System (ADS)

    Nkuissi Tchognia, Joël Hervé; Hartiti, Bouchaib; Ridah, Abderraouf; Ndjaka, Jean-Marie; Thevenin, Philippe

    2016-07-01

    Present research deals with the optimal deposition parameters configuration for the synthesis of Cu2ZnSnS4 (CZTS) thin films using the sol-gel method associated to spin coating on ordinary glass substrates without sulfurization. The Taguchi design with a L9 (34) orthogonal array, a signal-to-noise (S/N) ratio and an analysis of variance (ANOVA) are used to optimize the performance characteristic (optical band gap) of CZTS thin films. Four deposition parameters called factors namely the annealing temperature, the annealing time, the ratios Cu/(Zn + Sn) and Zn/Sn were chosen. To conduct the tests using the Taguchi method, three levels were chosen for each factor. The effects of the deposition parameters on structural and optical properties are studied. The determination of the most significant factors of the deposition process on optical properties of as-prepared films is also done. The results showed that the significant parameters are Zn/Sn ratio and the annealing temperature by applying the Taguchi method.

  2. A feasibility investigation for modeling and optimization of temperature in bone drilling using fuzzy logic and Taguchi optimization methodology.

    PubMed

    Pandey, Rupesh Kumar; Panda, Sudhansu Sekhar

    2014-11-01

    Drilling of bone is a common procedure in orthopedic surgery to produce hole for screw insertion to fixate the fracture devices and implants. The increase in temperature during such a procedure increases the chances of thermal invasion of bone which can cause thermal osteonecrosis resulting in the increase of healing time or reduction in the stability and strength of the fixation. Therefore, drilling of bone with minimum temperature is a major challenge for orthopedic fracture treatment. This investigation discusses the use of fuzzy logic and Taguchi methodology for predicting and minimizing the temperature produced during bone drilling. The drilling experiments have been conducted on bovine bone using Taguchi's L25 experimental design. A fuzzy model is developed for predicting the temperature during orthopedic drilling as a function of the drilling process parameters (point angle, helix angle, feed rate and cutting speed). Optimum bone drilling process parameters for minimizing the temperature are determined using Taguchi method. The effect of individual cutting parameters on the temperature produced is evaluated using analysis of variance. The fuzzy model using triangular and trapezoidal membership predicts the temperature within a maximum error of ±7%. Taguchi analysis of the obtained results determined the optimal drilling conditions for minimizing the temperature as A3B5C1.The developed system will simplify the tedious task of modeling and determination of the optimal process parameters to minimize the bone drilling temperature. It will reduce the risk of thermal osteonecrosis and can be very effective for the online condition monitoring of the process. © IMechE 2014.

  3. Robust Control Design for Uncertain Nonlinear Dynamic Systems

    NASA Technical Reports Server (NTRS)

    Kenny, Sean P.; Crespo, Luis G.; Andrews, Lindsey; Giesy, Daniel P.

    2012-01-01

    Robustness to parametric uncertainty is fundamental to successful control system design and as such it has been at the core of many design methods developed over the decades. Despite its prominence, most of the work on robust control design has focused on linear models and uncertainties that are non-probabilistic in nature. Recently, researchers have acknowledged this disparity and have been developing theory to address a broader class of uncertainties. This paper presents an experimental application of robust control design for a hybrid class of probabilistic and non-probabilistic parametric uncertainties. The experimental apparatus is based upon the classic inverted pendulum on a cart. The physical uncertainty is realized by a known additional lumped mass at an unknown location on the pendulum. This unknown location has the effect of substantially altering the nominal frequency and controllability of the nonlinear system, and in the limit has the capability to make the system neutrally stable and uncontrollable. Another uncertainty to be considered is a direct current motor parameter. The control design objective is to design a controller that satisfies stability, tracking error, control power, and transient behavior requirements for the largest range of parametric uncertainties. This paper presents an overview of the theory behind the robust control design methodology and the experimental results.

  4. A robust optimization methodology for preliminary aircraft design

    NASA Astrophysics Data System (ADS)

    Prigent, S.; Maréchal, P.; Rondepierre, A.; Druot, T.; Belleville, M.

    2016-05-01

    This article focuses on a robust optimization of an aircraft preliminary design under operational constraints. According to engineers' know-how, the aircraft preliminary design problem can be modelled as an uncertain optimization problem whose objective (the cost or the fuel consumption) is almost affine, and whose constraints are convex. It is shown that this uncertain optimization problem can be approximated in a conservative manner by an uncertain linear optimization program, which enables the use of the techniques of robust linear programming of Ben-Tal, El Ghaoui, and Nemirovski [Robust Optimization, Princeton University Press, 2009]. This methodology is then applied to two real cases of aircraft design and numerical results are presented.

  5. Towards robust optimal design of storm water systems

    NASA Astrophysics Data System (ADS)

    Marquez Calvo, Oscar; Solomatine, Dimitri

    2015-04-01

    In this study the focus is on the design of a storm water or a combined sewer system. Such a system should be capable to handle properly most of the storm to minimize the damages caused by flooding due to the lack of capacity of the system to cope with rain water at peak times. This problem is a multi-objective optimization problem: we have to take into account the minimization of the construction costs, the minimization of damage costs due to flooding, and possibly other criteria. One of the most important factors influencing the design of storm water systems is the expected amount of water to deal with. It is common that this infrastructure is developed with the capacity to cope with events that occur once in, say 10 or 20 years - so-called design rainfall events. However, rainfall is a random variable and such uncertainty typically is not taken explicitly into account in optimization. Rainfall design data is based on historical information of rainfalls, but many times this data is based on unreliable measures; or in not enough historical information; or as we know, the patterns of rainfall are changing regardless of historical information. There are also other sources of uncertainty influencing design, for example, leakages in the pipes and accumulation of sediments in pipes. In the context of storm water or combined sewer systems design or rehabilitation, robust optimization technique should be able to find the best design (or rehabilitation plan) within the available budget but taking into account uncertainty in those variables that were used to design the system. In this work we consider various approaches to robust optimization proposed by various authors (Gabrel, Murat, Thiele 2013; Beyer, Sendhoff 2007) and test a novel method ROPAR (Solomatine 2012) to analyze robustness. References Beyer, H.G., & Sendhoff, B. (2007). Robust optimization - A comprehensive survey. Comput. Methods Appl. Mech. Engrg., 3190-3218. Gabrel, V.; Murat, C., Thiele, A. (2014

  6. A comparative study of electrochemical machining process parameters by using GA and Taguchi method

    NASA Astrophysics Data System (ADS)

    Soni, S. K.; Thomas, B.

    2017-11-01

    In electrochemical machining quality of machined surface strongly depend on the selection of optimal parameter settings. This work deals with the application of Taguchi method and genetic algorithm using MATLAB to maximize the metal removal rate and minimize the surface roughness and overcut. In this paper a comparative study is presented for drilling of LM6 AL/B4C composites by comparing the significant impact of numerous machining process parameters such as, electrolyte concentration (g/l),machining voltage (v),frequency (hz) on the response parameters (surface roughness, material removal rate and over cut). Taguchi L27 orthogonal array was chosen in Minitab 17 software, for the investigation of experimental results and also multiobjective optimization done by genetic algorithm is employed by using MATLAB. After obtaining optimized results from Taguchi method and genetic algorithm, a comparative results are presented.

  7. Optimizing Cu(II) removal from aqueous solution by magnetic nanoparticles immobilized on activated carbon using Taguchi method.

    PubMed

    Ebrahimi Zarandi, Mohammad Javad; Sohrabi, Mahmoud Reza; Khosravi, Morteza; Mansouriieh, Nafiseh; Davallo, Mehran; Khosravan, Azita

    2016-01-01

    This study synthesized magnetic nanoparticles (Fe(3)O(4)) immobilized on activated carbon (AC) and used them as an effective adsorbent for Cu(II) removal from aqueous solution. The effect of three parameters, including the concentration of Cu(II), dosage of Fe(3)O(4)/AC magnetic nanocomposite and pH on the removal of Cu(II) using Fe(3)O(4)/AC nanocomposite were studied. In order to examine and describe the optimum condition for each of the mentioned parameters, Taguchi's optimization method was used in a batch system and L9 orthogonal array was used for the experimental design. The removal percentage (R%) of Cu(II) and uptake capacity (q) were transformed into an accurate signal-to-noise ratio (S/N) for a 'larger-the-better' response. Taguchi results, which were analyzed based on choosing the best run by examining the S/N, were statistically tested using analysis of variance; the tests showed that all the parameters' main effects were significant within a 95% confidence level. The best conditions for removal of Cu(II) were determined at pH of 7, nanocomposite dosage of 0.1 gL(-1) and initial Cu(II) concentration of 20 mg L(-1) at constant temperature of 25 °C. Generally, the results showed that the simple Taguchi's method is suitable to optimize the Cu(II) removal experiments.

  8. Robust decentralized power system controller design: Integrated approach

    NASA Astrophysics Data System (ADS)

    Veselý, Vojtech

    2017-09-01

    A unique approach to the design of gain scheduled controller (GSC) is presented. The proposed design procedure is based on the Bellman-Lyapunov equation, guaranteed cost and robust stability conditions using the parameter dependent quadratic stability approach. The obtained feasible design procedures for robust GSC design are in the form of BMI with guaranteed convex stability conditions. The obtained design results and their properties are illustrated in the simultaneously design of controllers for simple model (6-order) turbogenerator. The results of the obtained design procedure are a PI automatic voltage regulator (AVR) for synchronous generator, a PI governor controller and a power system stabilizer for excitation system.

  9. Towards Robust Designs Via Multiple-Objective Optimization Methods

    NASA Technical Reports Server (NTRS)

    Man Mohan, Rai

    2006-01-01

    Fabricating and operating complex systems involves dealing with uncertainty in the relevant variables. In the case of aircraft, flow conditions are subject to change during operation. Efficiency and engine noise may be different from the expected values because of manufacturing tolerances and normal wear and tear. Engine components may have a shorter life than expected because of manufacturing tolerances. In spite of the important effect of operating- and manufacturing-uncertainty on the performance and expected life of the component or system, traditional aerodynamic shape optimization has focused on obtaining the best design given a set of deterministic flow conditions. Clearly it is important to both maintain near-optimal performance levels at off-design operating conditions, and, ensure that performance does not degrade appreciably when the component shape differs from the optimal shape due to manufacturing tolerances and normal wear and tear. These requirements naturally lead to the idea of robust optimal design wherein the concept of robustness to various perturbations is built into the design optimization procedure. The basic ideas involved in robust optimal design will be included in this lecture. The imposition of the additional requirement of robustness results in a multiple-objective optimization problem requiring appropriate solution procedures. Typically the costs associated with multiple-objective optimization are substantial. Therefore efficient multiple-objective optimization procedures are crucial to the rapid deployment of the principles of robust design in industry. Hence the companion set of lecture notes (Single- and Multiple-Objective Optimization with Differential Evolution and Neural Networks ) deals with methodology for solving multiple-objective Optimization problems efficiently, reliably and with little user intervention. Applications of the methodologies presented in the companion lecture to robust design will be included here. The

  10. A Taguchi approach on optimal process control parameters for HDPE pipe extrusion process

    NASA Astrophysics Data System (ADS)

    Sharma, G. V. S. S.; Rao, R. Umamaheswara; Rao, P. Srinivasa

    2017-06-01

    High-density polyethylene (HDPE) pipes find versatile applicability for transportation of water, sewage and slurry from one place to another. Hence, these pipes undergo tremendous pressure by the fluid carried. The present work entails the optimization of the withstanding pressure of the HDPE pipes using Taguchi technique. The traditional heuristic methodology stresses on a trial and error approach and relies heavily upon the accumulated experience of the process engineers for determining the optimal process control parameters. This results in setting up of less-than-optimal values. Hence, there arouse a necessity to determine optimal process control parameters for the pipe extrusion process, which can ensure robust pipe quality and process reliability. In the proposed optimization strategy, the design of experiments (DoE) are conducted wherein different control parameter combinations are analyzed by considering multiple setting levels of each control parameter. The concept of signal-to-noise ratio ( S/ N ratio) is applied and ultimately optimum values of process control parameters are obtained as: pushing zone temperature of 166 °C, Dimmer speed at 08 rpm, and Die head temperature to be 192 °C. Confirmation experimental run is also conducted to verify the analysis and research result and values proved to be in synchronization with the main experimental findings and the withstanding pressure showed a significant improvement from 0.60 to 1.004 Mpa.

  11. Optimization of tribological performance of SiC embedded composite coating via Taguchi analysis approach

    NASA Astrophysics Data System (ADS)

    Maleque, M. A.; Bello, K. A.; Adebisi, A. A.; Akma, N.

    2017-03-01

    Tungsten inert gas (TIG) torch is one of the most recently used heat source for surface modification of engineering parts, giving similar results to the more expensive high power laser technique. In this study, ceramic-based embedded composite coating has been produced by precoated silicon carbide (SiC) powders on the AISI 4340 low alloy steel substrate using TIG welding torch process. A design of experiment based on Taguchi approach has been adopted to optimize the TIG cladding process parameters. The L9 orthogonal array and the signal-to-noise was used to study the effect of TIG welding parameters such as arc current, travelling speed, welding voltage and argon flow rate on tribological response behaviour (wear rate, surface roughness and wear track width). The objective of the study was to identify optimal design parameter that significantly minimizes each of the surface quality characteristics. The analysis of the experimental results revealed that the argon flow rate was found to be the most influential factor contributing to the minimum wear and surface roughness of the modified coating surface. On the other hand, the key factor in reducing wear scar is the welding voltage. Finally, a convenient and economical Taguchi approach used in this study was efficient to find out optimal factor settings for obtaining minimum wear rate, wear scar and surface roughness responses in TIG-coated surfaces.

  12. Use of Taguchi design of experiments to optimize and increase robustness of preliminary designs

    NASA Technical Reports Server (NTRS)

    Carrasco, Hector R.

    1992-01-01

    The research performed this summer includes the completion of work begun last summer in support of the Air Launched Personnel Launch System parametric study, providing support on the development of the test matrices for the plume experiments in the Plume Model Investigation Team Project, and aiding in the conceptual design of a lunar habitat. After the conclusion of last years Summer Program, the Systems Definition Branch continued with the Air Launched Personnel Launch System (ALPLS) study by running three experiments defined by L27 Orthogonal Arrays. Although the data was evaluated during the academic year, the analysis of variance and the final project review were completed this summer. The Plume Model Investigation Team (PLUMMIT) was formed by the Engineering Directorate to develop a consensus position on plume impingement loads and to validate plume flowfield models. In order to obtain a large number of individual correlated data sets for model validation, a series of plume experiments was planned. A preliminary 'full factorial' test matrix indicated that 73,024 jet firings would be necessary to obtain all of the information requested. As this was approximately 100 times more firings than the scheduled use of Vacuum Chamber A would permit, considerable effort was needed to reduce the test matrix and optimize it with respect to the specific objectives of the program. Part of the First Lunar Outpost Project deals with Lunar Habitat. Requirements for the habitat include radiation protection, a safe haven for occasional solar flare storms, an airlock module as well as consumables to support 34 extra vehicular activities during a 45 day mission. The objective for the proposed work was to collaborate with the Habitat Team on the development and reusability of the Logistics Modules.

  13. Robust Learning Control Design for Quantum Unitary Transformations.

    PubMed

    Wu, Chengzhi; Qi, Bo; Chen, Chunlin; Dong, Daoyi

    2017-12-01

    Robust control design for quantum unitary transformations has been recognized as a fundamental and challenging task in the development of quantum information processing due to unavoidable decoherence or operational errors in the experimental implementation of quantum operations. In this paper, we extend the systematic methodology of sampling-based learning control (SLC) approach with a gradient flow algorithm for the design of robust quantum unitary transformations. The SLC approach first uses a "training" process to find an optimal control strategy robust against certain ranges of uncertainties. Then a number of randomly selected samples are tested and the performance is evaluated according to their average fidelity. The approach is applied to three typical examples of robust quantum transformation problems including robust quantum transformations in a three-level quantum system, in a superconducting quantum circuit, and in a spin chain system. Numerical results demonstrate the effectiveness of the SLC approach and show its potential applications in various implementation of quantum unitary transformations.

  14. An analytic model for footprint dispersions and its application to mission design

    NASA Technical Reports Server (NTRS)

    Rao, J. R. Jagannatha; Chen, Yi-Chao

    1992-01-01

    This is the final report on our recent research activities that are complementary to those conducted by our colleagues, Professor Farrokh Mistree and students, in the context of the Taguchi method. We have studied the mathematical model that forms the basis of the Simulation and Optimization of Rocket Trajectories (SORT) program and developed an analytic method for determining mission reliability with a reduced number of flight simulations. This method can be incorporated in a design algorithm to mathematically optimize different performance measures of a mission, thus leading to a robust and easy-to-use methodology for mission planning and design.

  15. Robust spherical direct-drive design for NI

    NASA Astrophysics Data System (ADS)

    Masse, Laurent; Hurricane, O.; Michel, P.; Nora, R.; Tabak, M.; Lawrence Livermore Natl Lab Team

    2016-10-01

    Achieving ignition in a direct-drive or indirect-drive cryogenic implosion is a tremendous challenge. Both approaches need to deal with physic and technologic issues. During the past years, the indirect drive effort on the National Ignition Facility (NIF) has revealed unpredicted lost of performances that force to think to more robust designs and to dig into detailed physics aspects. Encouraging results have been obtained using a strong first shock during the implosion of CH ablator ignition capsules. These ``high-foot'' implosion results in a significantly lower ablation Rayleigh-Taylor instability growth than that of the NIC point design capsule. The trade-off with this design is a higher fuel adiabat that limits both fuel compression and theoretical capsule yield. The purpose of designing this capsule is to recover a more ideal one-dimensional implosion that is in closer agreement to simulation predictions. In the same spirit of spending energy on margin, at the coast of decreased performance, we are presenting here a study on ``robust'' spherical direct drive design for NIF. This 2-Shock direct drive pulse shape results in a high adiabat (>3) and low convergence (<17) implosion designed to produce a near 1D-like implosion. We take a particular attention to design a robust implosion with respect to long-wavelength non uniformity seeded by power imbalance and target offset. This work was performed under the auspices of the Lawrence Livermore National Security, LLC, (LLNS) under Contract No. DE-AC52-07NA27344.

  16. Multi-Response Optimization of Resin Finishing by Using a Taguchi-Based Grey Relational Analysis

    PubMed Central

    Shafiq, Faizan; Sarwar, Zahid; Jilani, Muhammad Munib; Cai, Yingjie

    2018-01-01

    In this study, the influence and optimization of the factors of a non-formaldehyde resin finishing process on cotton fabric using a Taguchi-based grey relational analysis were experimentally investigated. An L27 orthogonal array was selected for five parameters and three levels by applying Taguchi’s design of experiments. The Taguchi technique was coupled with a grey relational analysis to obtain a grey relational grade for evaluating multiple responses, i.e., crease recovery angle (CRA), tearing strength (TE), and whiteness index (WI). The optimum parameters (values) for resin finishing were the resin concentration (80 g·L−1), the polyethylene softener (40 g·L−1), the catalyst (25 g·L−1), the curing temperature (140 °C), and the curing time (2 min). The goodness-of-fit of the data was validated by an analysis of variance (ANOVA). The optimized sample was characterized by Fourier-transform infrared (FTIR) spectroscopy, thermogravimetric analysis (TGA), and scanning electron microscope (SEM) to better understand the structural details of the resin finishing process. The results showed an improved thermal stability and confirmed the presence of well deposited of resin on the optimized fabric surface. PMID:29543724

  17. On the Use of Statistics in Design and the Implications for Deterministic Computer Experiments

    NASA Technical Reports Server (NTRS)

    Simpson, Timothy W.; Peplinski, Jesse; Koch, Patrick N.; Allen, Janet K.

    1997-01-01

    Perhaps the most prevalent use of statistics in engineering design is through Taguchi's parameter and robust design -- using orthogonal arrays to compute signal-to-noise ratios in a process of design improvement. In our view, however, there is an equally exciting use of statistics in design that could become just as prevalent: it is the concept of metamodeling whereby statistical models are built to approximate detailed computer analysis codes. Although computers continue to get faster, analysis codes always seem to keep pace so that their computational time remains non-trivial. Through metamodeling, approximations of these codes are built that are orders of magnitude cheaper to run. These metamodels can then be linked to optimization routines for fast analysis, or they can serve as a bridge for integrating analysis codes across different domains. In this paper we first review metamodeling techniques that encompass design of experiments, response surface methodology, Taguchi methods, neural networks, inductive learning, and kriging. We discuss their existing applications in engineering design and then address the dangers of applying traditional statistical techniques to approximate deterministic computer analysis codes. We conclude with recommendations for the appropriate use of metamodeling techniques in given situations and how common pitfalls can be avoided.

  18. Advanced Design Methodology for Robust Aircraft Sizing and Synthesis

    NASA Technical Reports Server (NTRS)

    Mavris, Dimitri N.

    1997-01-01

    Contract efforts are focused on refining the Robust Design Methodology for Conceptual Aircraft Design. Robust Design Simulation (RDS) was developed earlier as a potential solution to the need to do rapid trade-offs while accounting for risk, conflict, and uncertainty. The core of the simulation revolved around Response Surface Equations as approximations of bounded design spaces. An ongoing investigation is concerned with the advantages of using Neural Networks in conceptual design. Thought was also given to the development of systematic way to choose or create a baseline configuration based on specific mission requirements. Expert system was developed, which selects aerodynamics, performance and weights model from several configurations based on the user's mission requirements for subsonic civil transport. The research has also resulted in a step-by-step illustration on how to use the AMV method for distribution generation and the search for robust design solutions to multivariate constrained problems.

  19. Mixing behavior of the rhombic micromixers over a wide Reynolds number range using Taguchi method and 3D numerical simulations.

    PubMed

    Chung, C K; Shih, T R; Chen, T C; Wu, B H

    2008-10-01

    A planar micromixer with rhombic microchannels and a converging-diverging element has been systematically investigated by the Taguchi method, CFD-ACE simulations and experiments. To reduce the footprint and extend the operation range of Reynolds number, Taguchi method was used to numerically study the performance of the micromixer in a L(9) orthogonal array. Mixing efficiency is prominently influenced by geometrical parameters and Reynolds number (Re). The four factors in a L(9) orthogonal array are number of rhombi, turning angle, width of the rhombic channel and width of the throat. The degree of sensitivity by Taguchi method can be ranked as: Number of rhombi > Width of the rhombic channel > Width of the throat > Turning angle of the rhombic channel. Increasing the number of rhombi, reducing the width of the rhombic channel and throat and lowering the turning angle resulted in better fluid mixing efficiency. The optimal design of the micromixer in simulations indicates over 90% mixing efficiency at both Re > or = 80 and Re < or = 0.1. Experimental results in the optimal simulations are consistent with the simulated one. This planar rhombic micromixer has simplified the complex fabrication process of the multi-layer or three-dimensional micromixers and improved the performance of a previous rhombic micromixer at a reduced footprint and lower Re.

  20. Robust Airfoil Optimization in High Resolution Design Space

    NASA Technical Reports Server (NTRS)

    Li, Wu; Padula, Sharon L.

    2003-01-01

    The robust airfoil shape optimization is a direct method for drag reduction over a given range of operating conditions and has three advantages: (1) it prevents severe degradation in the off-design performance by using a smart descent direction in each optimization iteration, (2) it uses a large number of B-spline control points as design variables yet the resulting airfoil shape is fairly smooth, and (3) it allows the user to make a trade-off between the level of optimization and the amount of computing time consumed. The robust optimization method is demonstrated by solving a lift-constrained drag minimization problem for a two-dimensional airfoil in viscous flow with a large number of geometric design variables. Our experience with robust optimization indicates that our strategy produces reasonable airfoil shapes that are similar to the original airfoils, but these new shapes provide drag reduction over the specified range of Mach numbers. We have tested this strategy on a number of advanced airfoil models produced by knowledgeable aerodynamic design team members and found that our strategy produces airfoils better or equal to any designs produced by traditional design methods.

  1. Robust crossfeed design for hovering rotorcraft. M.S. Thesis

    NASA Technical Reports Server (NTRS)

    Catapang, David R.

    1993-01-01

    Control law design for rotorcraft fly-by-wire systems normally attempts to decouple angular responses using fixed-gain crossfeeds. This approach can lead to poor decoupling over the frequency range of pilot inputs and increase the load on the feedback loops. In order to improve the decoupling performance, dynamic crossfeeds may be adopted. Moreover, because of the large changes that occur in rotorcraft dynamics due to small changes about the nominal design condition, especially for near-hovering flight, the crossfeed design must be 'robust.' A new low-order matching method is presented here to design robost crossfeed compensators for multi-input, multi-output (MIMO) systems. The technique identifies degrees-of-freedom that can be decoupled using crossfeeds, given an anticipated set of parameter variations for the range of flight conditions of concern. Cross-coupling is then reduced for degrees-of-freedom that can use crossfeed compensation by minimizing off-axis response magnitude average and variance. Results are presented for the analysis of pitch, roll, yaw, and heave coupling of the UH-60 Black Hawk helicopter in near-hovering flight. Robust crossfeeds are designed that show significant improvement in decoupling performance and robustness over nominal, single design point, compensators. The design method and results are presented in an easily-used graphical format that lends significant physical insight to the design procedure. This plant pre-compensation technique is an appropriate preliminary step to the design of robust feedback control laws for rotorcraft.

  2. Manufacturing Research: Self-Directed Control

    DTIC Science & Technology

    1991-01-01

    reduce this sensitivity. SDO is performing Taguchi’s parameter design . 1-13 Statistical Process Control SPC techniques will be used to monitor the process...Florida,R.E. Krieger Pub. Co., 1988. Dehnad, Khowrow, Quality Control . Robust Design . and the Taguchi Method, Pacific Grove, California, Wadsworth... control system. This turns out to be a non -trivial exercise. A human operator can see an event occur (such as the vessel pressurizing above its setpoint

  3. Robust linear quadratic designs with respect to parameter uncertainty

    NASA Technical Reports Server (NTRS)

    Douglas, Joel; Athans, Michael

    1992-01-01

    The authors derive a linear quadratic regulator (LQR) which is robust to parametric uncertainty by using the overbounding method of I. R. Petersen and C. V. Hollot (1986). The resulting controller is determined from the solution of a single modified Riccati equation. It is shown that, when applied to a structural system, the controller gains add robustness by minimizing the potential energy of uncertain stiffness elements, and minimizing the rate of dissipation of energy through uncertain damping elements. A worst-case disturbance in the direction of the uncertainty is also considered. It is proved that performance robustness has been increased with the robust LQR when compared to a mismatched LQR design where the controller is designed on the nominal system, but applied to the actual uncertain system.

  4. Robust Control Design for Systems With Probabilistic Uncertainty

    NASA Technical Reports Server (NTRS)

    Crespo, Luis G.; Kenny, Sean P.

    2005-01-01

    This paper presents a reliability- and robustness-based formulation for robust control synthesis for systems with probabilistic uncertainty. In a reliability-based formulation, the probability of violating design requirements prescribed by inequality constraints is minimized. In a robustness-based formulation, a metric which measures the tendency of a random variable/process to cluster close to a target scalar/function is minimized. A multi-objective optimization procedure, which combines stability and performance requirements in time and frequency domains, is used to search for robustly optimal compensators. Some of the fundamental differences between the proposed strategy and conventional robust control methods are: (i) unnecessary conservatism is eliminated since there is not need for convex supports, (ii) the most likely plants are favored during synthesis allowing for probabilistic robust optimality, (iii) the tradeoff between robust stability and robust performance can be explored numerically, (iv) the uncertainty set is closely related to parameters with clear physical meaning, and (v) compensators with improved robust characteristics for a given control structure can be synthesized.

  5. Design and implementation of robust controllers for a gait trainer.

    PubMed

    Wang, F C; Yu, C H; Chou, T Y

    2009-08-01

    This paper applies robust algorithms to control an active gait trainer for children with walking disabilities. Compared with traditional rehabilitation procedures, in which two or three trainers are required to assist the patient, a motor-driven mechanism was constructed to improve the efficiency of the procedures. First, a six-bar mechanism was designed and constructed to mimic the trajectory of children's ankles in walking. Second, system identification techniques were applied to obtain system transfer functions at different operating points by experiments. Third, robust control algorithms were used to design Hinfinity robust controllers for the system. Finally, the designed controllers were implemented to verify experimentally the system performance. From the results, the proposed robust control strategies are shown to be effective.

  6. Rolling bearing fault diagnosis and health assessment using EEMD and the adjustment Mahalanobis-Taguchi system

    NASA Astrophysics Data System (ADS)

    Chen, Junxun; Cheng, Longsheng; Yu, Hui; Hu, Shaolin

    2018-01-01

    ABSTRACTSFor the timely identification of the potential faults of a rolling bearing and to observe its health condition intuitively and accurately, a novel fault diagnosis and health assessment model for a rolling bearing based on the ensemble empirical mode decomposition (EEMD) method and the adjustment Mahalanobis-<span class="hlt">Taguchi</span> system (AMTS) method is proposed. The specific steps are as follows: First, the vibration signal of a rolling bearing is decomposed by EEMD, and the extracted features are used as the input vectors of AMTS. Then, the AMTS method, which is <span class="hlt">designed</span> to overcome the shortcomings of the traditional Mahalanobis-<span class="hlt">Taguchi</span> system and to extract the key features, is proposed for fault diagnosis. Finally, a type of HI concept is proposed according to the results of the fault diagnosis to accomplish the health assessment of a bearing in its life cycle. To validate the superiority of the developed method proposed approach, it is compared with other recent method and proposed methodology is successfully validated on a vibration data-set acquired from seeded defects and from an accelerated life test. The results show that this method represents the actual situation well and is able to accurately and effectively identify the fault type.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27885074','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27885074"><span>Developing an Optimum Protocol for Thermoluminescence Dosimetry with GR-200 Chips using <span class="hlt">Taguchi</span> Method.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sadeghi, Maryam; Faghihi, Reza; Sina, Sedigheh</p> <p>2017-06-15</p> <p>Thermoluminescence dosimetry (TLD) is a powerful technique with wide applications in personal, environmental and clinical dosimetry. The optimum annealing, storage and reading protocols are very effective in accuracy of TLD response. The purpose of this study is to obtain an optimum protocol for GR-200; LiF: Mg, Cu, P, by optimizing the effective parameters, to increase the reliability of the TLD response using <span class="hlt">Taguchi</span> method. <span class="hlt">Taguchi</span> method has been used in this study for optimization of annealing, storage and reading protocols of the TLDs. A number of 108 GR-200 chips were divided into 27 groups, each containing four chips. The TLDs were exposed to three different doses, and stored, annealed and read out by different procedures as suggested by <span class="hlt">Taguchi</span> Method. By comparing the signal-to-noise ratios the optimum dosimetry procedure was obtained. According to the results, the optimum values for annealing temperature (°C), Annealing Time (s), Annealing to Exposure time (d), Exposure to Readout time (d), Pre-heat Temperature (°C), Pre-heat Time (s), Heating Rate (°C/s), Maximum Temperature of Readout (°C), readout time (s) and Storage Temperature (°C) are 240, 90, 1, 2, 50, 0, 15, 240, 13 and -20, respectively. Using the optimum protocol, an efficient glow curve with low residual signals can be achieved. Using optimum protocol obtained by <span class="hlt">Taguchi</span> method, the dosimetry can be effectively performed with great accuracy. © The Author 2016. Published by Oxford University Press. All rights reserved. For Permissions, please email: journals.permissions@oup.com.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19840056958&hterms=detection+systems&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Ddetection%2Bsystems','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19840056958&hterms=detection+systems&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Ddetection%2Bsystems"><span>Analytical redundancy and the <span class="hlt">design</span> of <span class="hlt">robust</span> failure detection systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chow, E. Y.; Willsky, A. S.</p> <p>1984-01-01</p> <p>The Failure Detection and Identification (FDI) process is viewed as consisting of two stages: residual generation and decision making. It is argued that a <span class="hlt">robust</span> FDI system can be achieved by <span class="hlt">designing</span> a <span class="hlt">robust</span> residual generation process. Analytical redundancy, the basis for residual generation, is characterized in terms of a parity space. Using the concept of parity relations, residuals can be generated in a number of ways and the <span class="hlt">design</span> of a <span class="hlt">robust</span> residual generation process can be formulated as a minimax optimization problem. An example is included to illustrate this <span class="hlt">design</span> methodology. Previously announcedd in STAR as N83-20653</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20020077985','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20020077985"><span><span class="hlt">Designing</span> for Damage: <span class="hlt">Robust</span> Flight Control <span class="hlt">Design</span> using Sliding Mode Techniques</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Vetter, T. K.; Wells, S. R.; Hess, Ronald A.; Bacon, Barton (Technical Monitor); Davidson, John (Technical Monitor)</p> <p>2002-01-01</p> <p>A brief review of sliding model control is undertaken, with particular emphasis upon the effects of neglected parasitic dynamics. Sliding model control <span class="hlt">design</span> is interpreted in the frequency domain. The inclusion of asymptotic observers and control 'hedging' is shown to reduce the effects of neglected parasitic dynamics. An investigation into the application of observer-based sliding mode control to the <span class="hlt">robust</span> longitudinal control of a highly unstable is described. The sliding mode controller is shown to exhibit stability and performance <span class="hlt">robustness</span> superior to that of a classical loop-shaped <span class="hlt">design</span> when significant changes in vehicle and actuator dynamics are employed to model airframe damage.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22751850','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22751850"><span>Neutralization of red mud with pickling waste liquor using <span class="hlt">Taguchi</span>'s <span class="hlt">design</span> of experimental methodology.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Rai, Suchita; Wasewar, Kailas L; Lataye, Dilip H; Mishra, Rajshekhar S; Puttewar, Suresh P; Chaddha, Mukesh J; Mahindiran, P; Mukhopadhyay, Jyoti</p> <p>2012-09-01</p> <p>'Red mud' or 'bauxite residue', a waste generated from alumina refinery is highly alkaline in nature with a pH of 10.5-12.5. Red mud poses serious environmental problems such as alkali seepage in ground water and alkaline dust generation. One of the options to make red mud less hazardous and environmentally benign is its neutralization with acid or an acidic waste. Hence, in the present study, neutralization of alkaline red mud was carried out using a highly acidic waste (pickling waste liquor). Pickling waste liquor is a mixture of strong acids used for descaling or cleaning the surfaces in steel making industry. The aim of the study was to look into the feasibility of neutralization process of the two wastes using <span class="hlt">Taguchi</span>'s <span class="hlt">design</span> of experimental methodology. This would make both the wastes less hazardous and safe for disposal. The effect of slurry solids, volume of pickling liquor, stirring time and temperature on the neutralization process were investigated. The analysis of variance (ANOVA) shows that the volume of the pickling liquor is the most significant parameter followed by quantity of red mud with 69.18% and 18.48% contribution each respectively. Under the optimized parameters, pH value of 7 can be achieved by mixing the two wastes. About 25-30% of the total soda from the red mud is being neutralized and alkalinity is getting reduced by 80-85%. Mineralogy and morphology of the neutralized red mud have also been studied. The data presented will be useful in view of environmental concern of red mud disposal.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009EJASP2009...74U','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009EJASP2009...74U"><span><span class="hlt">Robust</span> THP Transceiver <span class="hlt">Designs</span> for Multiuser MIMO Downlink with Imperfect CSIT</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ubaidulla, P.; Chockalingam, A.</p> <p>2009-12-01</p> <p>We present <span class="hlt">robust</span> joint nonlinear transceiver <span class="hlt">designs</span> for multiuser multiple-input multiple-output (MIMO) downlink in the presence of imperfections in the channel state information at the transmitter (CSIT). The base station (BS) is equipped with multiple transmit antennas, and each user terminal is equipped with one or more receive antennas. The BS employs Tomlinson-Harashima precoding (THP) for interuser interference precancellation at the transmitter. We consider <span class="hlt">robust</span> transceiver <span class="hlt">designs</span> that jointly optimize the transmit THP filters and receive filter for two models of CSIT errors. The first model is a stochastic error (SE) model, where the CSIT error is Gaussian-distributed. This model is applicable when the CSIT error is dominated by channel estimation error. In this case, the proposed <span class="hlt">robust</span> transceiver <span class="hlt">design</span> seeks to minimize a stochastic function of the sum mean square error (SMSE) under a constraint on the total BS transmit power. We propose an iterative algorithm to solve this problem. The other model we consider is a norm-bounded error (NBE) model, where the CSIT error can be specified by an uncertainty set. This model is applicable when the CSIT error is dominated by quantization errors. In this case, we consider a worst-case <span class="hlt">design</span>. For this model, we consider <span class="hlt">robust</span> (i) minimum SMSE, (ii) MSE-constrained, and (iii) MSE-balancing transceiver <span class="hlt">designs</span>. We propose iterative algorithms to solve these problems, wherein each iteration involves a pair of semidefinite programs (SDPs). Further, we consider an extension of the proposed algorithm to the case with per-antenna power constraints. We evaluate the <span class="hlt">robustness</span> of the proposed algorithms to imperfections in CSIT through simulation, and show that the proposed <span class="hlt">robust</span> <span class="hlt">designs</span> outperform nonrobust <span class="hlt">designs</span> as well as <span class="hlt">robust</span> linear transceiver <span class="hlt">designs</span> reported in the recent literature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18672451','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18672451"><span>Two challenges in embedded systems <span class="hlt">design</span>: predictability and <span class="hlt">robustness</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Henzinger, Thomas A</p> <p>2008-10-28</p> <p>I discuss two main challenges in embedded systems <span class="hlt">design</span>: the challenge to build predictable systems, and that to build <span class="hlt">robust</span> systems. I suggest how predictability can be formalized as a form of determinism, and <span class="hlt">robustness</span> as a form of continuity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMNH51B1883S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMNH51B1883S"><span><span class="hlt">Designing</span> Flood Management Systems for Joint Economic and Ecological <span class="hlt">Robustness</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Spence, C. M.; Grantham, T.; Brown, C. M.; Poff, N. L.</p> <p>2015-12-01</p> <p>Freshwater ecosystems across the United States are threatened by hydrologic change caused by water management operations and non-stationary climate trends. Nonstationary hydrology also threatens flood management systems' performance. Ecosystem managers and flood risk managers need tools to <span class="hlt">design</span> systems that achieve flood risk reduction objectives while sustaining ecosystem functions and services in an uncertain hydrologic future. <span class="hlt">Robust</span> optimization is used in water resources engineering to guide system <span class="hlt">design</span> under climate change uncertainty. Using principles introduced by Eco-Engineering Decision Scaling (EEDS), we extend <span class="hlt">robust</span> optimization techniques to <span class="hlt">design</span> flood management systems that meet both economic and ecological goals simultaneously across a broad range of future climate conditions. We use three alternative <span class="hlt">robustness</span> indices to identify flood risk management solutions that preserve critical ecosystem functions in a case study from the Iowa River, where recent severe flooding has tested the limits of the existing flood management system. We seek <span class="hlt">design</span> modifications to the system that both reduce expected cost of flood damage while increasing ecologically beneficial inundation of riparian floodplains across a wide range of plausible climate futures. The first <span class="hlt">robustness</span> index measures <span class="hlt">robustness</span> as the fraction of potential climate scenarios in which both engineering and ecological performance goals are met, implicitly weighting each climate scenario equally. The second index builds on the first by using climate projections to weight each climate scenario, prioritizing acceptable performance in climate scenarios most consistent with climate projections. The last index measures <span class="hlt">robustness</span> as mean performance across all climate scenarios, but penalizes scenarios with worse performance than average, rewarding consistency. Results stemming from alternate <span class="hlt">robustness</span> indices reflect implicit assumptions about attitudes toward risk and reveal the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013SPIE.8684E..0QL','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013SPIE.8684E..0QL"><span>A novel methodology for building <span class="hlt">robust</span> <span class="hlt">design</span> rules by using <span class="hlt">design</span> based metrology (DBM)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lee, Myeongdong; Choi, Seiryung; Choi, Jinwoo; Kim, Jeahyun; Sung, Hyunju; Yeo, Hyunyoung; Shim, Myoungseob; Jin, Gyoyoung; Chung, Eunseung; Roh, Yonghan</p> <p>2013-03-01</p> <p>This paper addresses a methodology for building <span class="hlt">robust</span> <span class="hlt">design</span> rules by using <span class="hlt">design</span> based metrology (DBM). Conventional method for building <span class="hlt">design</span> rules has been using a simulation tool and a simple pattern spider mask. At the early stage of the device, the estimation of simulation tool is poor. And the evaluation of the simple pattern spider mask is rather subjective because it depends on the experiential judgment of an engineer. In this work, we <span class="hlt">designed</span> a huge number of pattern situations including various 1D and 2D <span class="hlt">design</span> structures. In order to overcome the difficulties of inspecting many types of patterns, we introduced <span class="hlt">Design</span> Based Metrology (DBM) of Nano Geometry Research, Inc. And those mass patterns could be inspected at a fast speed with DBM. We also carried out quantitative analysis on PWQ silicon data to estimate process variability. Our methodology demonstrates high speed and accuracy for building <span class="hlt">design</span> rules. All of test patterns were inspected within a few hours. Mass silicon data were handled with not personal decision but statistical processing. From the results, <span class="hlt">robust</span> <span class="hlt">design</span> rules are successfully verified and extracted. Finally we found out that our methodology is appropriate for building <span class="hlt">robust</span> <span class="hlt">design</span> rules.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26719136','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26719136"><span>Improving the Glucose Meter Error Grid With the <span class="hlt">Taguchi</span> Loss Function.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Krouwer, Jan S</p> <p>2016-07-01</p> <p>Glucose meters often have similar performance when compared by error grid analysis. This is one reason that other statistics such as mean absolute relative deviation (MARD) are used to further differentiate performance. The problem with MARD is that too much information is lost. But additional information is available within the A zone of an error grid by using the <span class="hlt">Taguchi</span> loss function. Applying the <span class="hlt">Taguchi</span> loss function gives each glucose meter difference from reference a value ranging from 0 (no error) to 1 (error reaches the A zone limit). Values are averaged over all data which provides an indication of risk of an incorrect medical decision. This allows one to differentiate glucose meter performance for the common case where meters have a high percentage of values in the A zone and no values beyond the B zone. Examples are provided using simulated data. © 2015 Diabetes Technology Society.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..306a2099N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..306a2099N"><span>Factors Affecting Optimal Surface Roughness of AISI 4140 Steel in Turning Operation Using <span class="hlt">Taguchi</span> Experiment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Novareza, O.; Sulistiyarini, D. H.; Wiradmoko, R.</p> <p>2018-02-01</p> <p>This paper presents the result of using <span class="hlt">Taguchi</span> method in turning process of medium carbon steel of AISI 4140. The primary concern is to find the optimal surface roughness after turning process. The <span class="hlt">taguchi</span> method is used to get a combination of factors and factor levels in order to get the optimum surface roughness level. Four important factors with three levels were used in experiment based on <span class="hlt">Taguchi</span> method. A number of 27 experiments were carried out during the research and analysed using analysis of variance (ANOVA) method. The result of surface finish was determined in Ra type surface roughness. The depth of cut was found to be the most important factors for reducing the surface roughness of AISI 4140 steel. On the contrary, the other important factors i.e. spindle speed and rake side angle of the tool were proven to be less factors that affecting the surface finish. It is interesting to see the effect of coolant composition that gained the second important factors to reduce the roughness. It may need further research to explain this result.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JIEI...11..459K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JIEI...11..459K"><span>Multiple performance characteristics optimization for Al 7075 on electric discharge drilling by <span class="hlt">Taguchi</span> grey relational theory</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Khanna, Rajesh; Kumar, Anish; Garg, Mohinder Pal; Singh, Ajit; Sharma, Neeraj</p> <p>2015-12-01</p> <p>Electric discharge drill machine (EDDM) is a spark erosion process to produce micro-holes in conductive materials. This process is widely used in aerospace, medical, dental and automobile industries. As for the performance evaluation of the electric discharge drilling machine, it is very necessary to study the process parameters of machine tool. In this research paper, a brass rod 2 mm diameter was selected as a tool electrode. The experiments generate output responses such as tool wear rate (TWR). The best parameters such as pulse on-time, pulse off-time and water pressure were studied for best machining characteristics. This investigation presents the use of <span class="hlt">Taguchi</span> approach for better TWR in drilling of Al-7075. A plan of experiments, based on L27 <span class="hlt">Taguchi</span> <span class="hlt">design</span> method, was selected for drilling of material. Analysis of variance (ANOVA) shows the percentage contribution of the control factor in the machining of Al-7075 in EDDM. The optimal combination levels and the significant drilling parameters on TWR were obtained. The optimization results showed that the combination of maximum pulse on-time and minimum pulse off-time gives maximum MRR.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.fs.usda.gov/treesearch/pubs/45062','TREESEARCH'); return false;" href="https://www.fs.usda.gov/treesearch/pubs/45062"><span><span class="hlt">Robust</span> network <span class="hlt">design</span> for multispecies conservation</span></a></p> <p><a target="_blank" href="http://www.fs.usda.gov/treesearch/">Treesearch</a></p> <p>Ronan Le Bras; Bistra Dilkina; Yexiang Xue; Carla P. Gomes; Kevin S. McKelvey; Michael K. Schwartz; Claire A. Montgomery</p> <p>2013-01-01</p> <p>Our work is motivated by an important network <span class="hlt">design</span> application in computational sustainability concerning wildlife conservation. In the face of human development and climate change, it is important that conservation plans for protecting landscape connectivity exhibit certain level of <span class="hlt">robustness</span>. While previous work has focused on conservation strategies that result...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980021298','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980021298"><span><span class="hlt">Robust</span>, Decoupled, Flight Control <span class="hlt">Design</span> with Rate Saturating Actuators</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Snell, S. A.; Hess, R. A.</p> <p>1997-01-01</p> <p>Techniques for the <span class="hlt">design</span> of control systems for manually controlled, high-performance aircraft must provide the following: (1) multi-input, multi-output (MIMO) solutions, (2) acceptable handling qualities including no tendencies for pilot-induced oscillations, (3) a tractable approach for compensator <span class="hlt">design</span>, (4) performance and stability <span class="hlt">robustness</span> in the presence of significant plant uncertainty, and (5) performance and stability <span class="hlt">robustness</span> in the presence actuator saturation (particularly rate saturation). A <span class="hlt">design</span> technique built upon Quantitative Feedback Theory is offered as a candidate methodology which can provide flight control systems meeting these requirements, and do so over a considerable part of the flight envelope. An example utilizing a simplified model of a supermaneuverable fighter aircraft demonstrates the proposed <span class="hlt">design</span> methodology.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3237015','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3237015"><span><span class="hlt">Robust</span> <span class="hlt">Design</span> of Biological Circuits: Evolutionary Systems Biology Approach</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chen, Bor-Sen; Hsu, Chih-Yuan; Liou, Jing-Jia</p> <p>2011-01-01</p> <p>Artificial gene circuits have been proposed to be embedded into microbial cells that function as switches, timers, oscillators, and the Boolean logic gates. Building more complex systems from these basic gene circuit components is one key advance for biologic circuit <span class="hlt">design</span> and synthetic biology. However, the behavior of bioengineered gene circuits remains unstable and uncertain. In this study, a nonlinear stochastic system is proposed to model the biological systems with intrinsic parameter fluctuations and environmental molecular noise from the cellular context in the host cell. Based on evolutionary systems biology algorithm, the <span class="hlt">design</span> parameters of target gene circuits can evolve to specific values in order to <span class="hlt">robustly</span> track a desired biologic function in spite of intrinsic and environmental noise. The fitness function is selected to be inversely proportional to the tracking error so that the evolutionary biological circuit can achieve the optimal tracking mimicking the evolutionary process of a gene circuit. Finally, several <span class="hlt">design</span> examples are given in silico with the Monte Carlo simulation to illustrate the <span class="hlt">design</span> procedure and to confirm the <span class="hlt">robust</span> performance of the proposed <span class="hlt">design</span> method. The result shows that the <span class="hlt">designed</span> gene circuits can <span class="hlt">robustly</span> track desired behaviors with minimal errors even with nontrivial intrinsic and external noise. PMID:22187523</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_6 --> <div id="page_7" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="121"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22187523','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22187523"><span><span class="hlt">Robust</span> <span class="hlt">design</span> of biological circuits: evolutionary systems biology approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Bor-Sen; Hsu, Chih-Yuan; Liou, Jing-Jia</p> <p>2011-01-01</p> <p>Artificial gene circuits have been proposed to be embedded into microbial cells that function as switches, timers, oscillators, and the Boolean logic gates. Building more complex systems from these basic gene circuit components is one key advance for biologic circuit <span class="hlt">design</span> and synthetic biology. However, the behavior of bioengineered gene circuits remains unstable and uncertain. In this study, a nonlinear stochastic system is proposed to model the biological systems with intrinsic parameter fluctuations and environmental molecular noise from the cellular context in the host cell. Based on evolutionary systems biology algorithm, the <span class="hlt">design</span> parameters of target gene circuits can evolve to specific values in order to <span class="hlt">robustly</span> track a desired biologic function in spite of intrinsic and environmental noise. The fitness function is selected to be inversely proportional to the tracking error so that the evolutionary biological circuit can achieve the optimal tracking mimicking the evolutionary process of a gene circuit. Finally, several <span class="hlt">design</span> examples are given in silico with the Monte Carlo simulation to illustrate the <span class="hlt">design</span> procedure and to confirm the <span class="hlt">robust</span> performance of the proposed <span class="hlt">design</span> method. The result shows that the <span class="hlt">designed</span> gene circuits can <span class="hlt">robustly</span> track desired behaviors with minimal errors even with nontrivial intrinsic and external noise.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5811023','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5811023"><span>Optimization of <span class="hlt">robustness</span> of interdependent network controllability by redundant <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2018-01-01</p> <p>Controllability of complex networks has been a hot topic in recent years. Real networks regarded as interdependent networks are always coupled together by multiple networks. The cascading process of interdependent networks including interdependent failure and overload failure will destroy the <span class="hlt">robustness</span> of controllability for the whole network. Therefore, the optimization of the <span class="hlt">robustness</span> of interdependent network controllability is of great importance in the research area of complex networks. In this paper, based on the model of interdependent networks constructed first, we determine the cascading process under different proportions of node attacks. Then, the structural controllability of interdependent networks is measured by the minimum driver nodes. Furthermore, we propose a parameter which can be obtained by the structure and minimum driver set of interdependent networks under different proportions of node attacks and analyze the <span class="hlt">robustness</span> for interdependent network controllability. Finally, we optimize the <span class="hlt">robustness</span> of interdependent network controllability by redundant <span class="hlt">design</span> including node backup and redundancy edge backup and improve the redundant <span class="hlt">design</span> by proposing different strategies according to their cost. Comparative strategies of redundant <span class="hlt">design</span> are conducted to find the best strategy. Results shows that node backup and redundancy edge backup can indeed decrease those nodes suffering from failure and improve the <span class="hlt">robustness</span> of controllability. Considering the cost of redundant <span class="hlt">design</span>, we should choose BBS (betweenness-based strategy) or DBS (degree based strategy) for node backup and HDF(high degree first) for redundancy edge backup. Above all, our proposed strategies are feasible and effective at improving the <span class="hlt">robustness</span> of interdependent network controllability. PMID:29438426</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150002820','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150002820"><span>Enabling Rapid and <span class="hlt">Robust</span> Structural Analysis During Conceptual <span class="hlt">Design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Eldred, Lloyd B.; Padula, Sharon L.; Li, Wu</p> <p>2015-01-01</p> <p>This paper describes a multi-year effort to add a structural analysis subprocess to a supersonic aircraft conceptual <span class="hlt">design</span> process. The desired capabilities include parametric geometry, automatic finite element mesh generation, static and aeroelastic analysis, and structural sizing. The paper discusses implementation details of the new subprocess, captures lessons learned, and suggests future improvements. The subprocess quickly compares concepts and <span class="hlt">robustly</span> handles large changes in wing or fuselage geometry. The subprocess can rank concepts with regard to their structural feasibility and can identify promising regions of the <span class="hlt">design</span> space. The automated structural analysis subprocess is deemed <span class="hlt">robust</span> and rapid enough to be included in multidisciplinary conceptual <span class="hlt">design</span> and optimization studies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EnOp...47..287Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EnOp...47..287Z"><span>Multi-point objective-oriented sequential sampling strategy for constrained <span class="hlt">robust</span> <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhu, Ping; Zhang, Siliang; Chen, Wei</p> <p>2015-03-01</p> <p>Metamodelling techniques are widely used to approximate system responses of expensive simulation models. In association with the use of metamodels, objective-oriented sequential sampling methods have been demonstrated to be effective in balancing the need for searching an optimal solution versus reducing the metamodelling uncertainty. However, existing infilling criteria are developed for deterministic problems and restricted to one sampling point in one iteration. To exploit the use of multiple samples and identify the true <span class="hlt">robust</span> solution in fewer iterations, a multi-point objective-oriented sequential sampling strategy is proposed for constrained <span class="hlt">robust</span> <span class="hlt">design</span> problems. In this article, earlier development of objective-oriented sequential sampling strategy for unconstrained <span class="hlt">robust</span> <span class="hlt">design</span> is first extended to constrained problems. Next, a double-loop multi-point sequential sampling strategy is developed. The proposed methods are validated using two mathematical examples followed by a highly nonlinear automotive crashworthiness <span class="hlt">design</span> example. The results show that the proposed method can mitigate the effect of both metamodelling uncertainty and <span class="hlt">design</span> uncertainty, and identify the <span class="hlt">robust</span> <span class="hlt">design</span> solution more efficiently than the single-point sequential sampling approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26106505','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26106505"><span>An Efficient <span class="hlt">Taguchi</span> Approach for the Performance Optimization of Health, Safety, Environment and Ergonomics in Generation Companies.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Azadeh, Ali; Sheikhalishahi, Mohammad</p> <p>2015-06-01</p> <p>A unique framework for performance optimization of generation companies (GENCOs) based on health, safety, environment, and ergonomics (HSEE) indicators is presented. To rank this sector of industry, the combination of data envelopment analysis (DEA), principal component analysis (PCA), and <span class="hlt">Taguchi</span> are used for all branches of GENCOs. These methods are applied in an integrated manner to measure the performance of GENCO. The preferred model between DEA, PCA, and <span class="hlt">Taguchi</span> is selected based on sensitivity analysis and maximum correlation between rankings. To achieve the stated objectives, noise is introduced into input data. The results show that <span class="hlt">Taguchi</span> outperforms other methods. Moreover, a comprehensive experiment is carried out to identify the most influential factor for ranking GENCOs. The approach developed in this study could be used for continuous assessment and improvement of GENCO's performance in supplying energy with respect to HSEE factors. The results of such studies would help managers to have better understanding of weak and strong points in terms of HSEE factors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20020013941','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20020013941"><span>A <span class="hlt">Robust</span> <span class="hlt">Design</span> Methodology for Optimal Microscale Secondary Flow Control in Compact Inlet Diffusers</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anderson, Bernhard H.; Keller, Dennis J.</p> <p>2001-01-01</p> <p>It is the purpose of this study to develop an economical <span class="hlt">Robust</span> <span class="hlt">design</span> methodology for microscale secondary flow control in compact inlet diffusers. To illustrate the potential of economical <span class="hlt">Robust</span> <span class="hlt">Design</span> methodology, two different mission strategies were considered for the subject inlet, namely Maximum Performance and Maximum HCF Life Expectancy. The Maximum Performance mission maximized total pressure recovery while the Maximum HCF Life Expectancy mission minimized the mean of the first five Fourier harmonic amplitudes, i.e., 'collectively' reduced all the harmonic 1/2 amplitudes of engine face distortion. Each of the mission strategies was subject to a low engine face distortion constraint, i.e., DC60<0.10, which is a level acceptable for commercial engines. For each of these missions strategies, an 'Optimal <span class="hlt">Robust</span>' (open loop control) and an 'Optimal Adaptive' (closed loop control) installation was <span class="hlt">designed</span> over a twenty degree angle-of-incidence range. The Optimal <span class="hlt">Robust</span> installation used economical <span class="hlt">Robust</span> <span class="hlt">Design</span> methodology to arrive at a single <span class="hlt">design</span> which operated over the entire angle-of-incident range (open loop control). The Optimal Adaptive installation optimized all the <span class="hlt">design</span> parameters at each angle-of-incidence. Thus, the Optimal Adaptive installation would require a closed loop control system to sense a proper signal for each effector and modify that effector device, whether mechanical or fluidic, for optimal inlet performance. In general, the performance differences between the Optimal Adaptive and Optimal <span class="hlt">Robust</span> installation <span class="hlt">designs</span> were found to be marginal. This suggests, however, that Optimal <span class="hlt">Robust</span> open loop installation <span class="hlt">designs</span> can be very competitive with Optimal Adaptive close loop <span class="hlt">designs</span>. Secondary flow control in inlets is inherently <span class="hlt">robust</span>, provided it is optimally <span class="hlt">designed</span>. Therefore, the new methodology presented in this paper, combined array 'Lower Order' approach to <span class="hlt">Robust</span> DOE, offers the aerodynamicist a very viable and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030020833','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030020833"><span>Reducing <span class="hlt">Design</span> Risk Using <span class="hlt">Robust</span> <span class="hlt">Design</span> Methods: A Dual Response Surface Approach</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Unal, Resit; Yeniay, Ozgur; Lepsch, Roger A. (Technical Monitor)</p> <p>2003-01-01</p> <p>Space transportation system conceptual <span class="hlt">design</span> is a multidisciplinary process containing considerable element of risk. Risk here is defined as the variability in the estimated (output) performance characteristic of interest resulting from the uncertainties in the values of several disciplinary <span class="hlt">design</span> and/or operational parameters. Uncertainties from one discipline (and/or subsystem) may propagate to another, through linking parameters and the final system output may have a significant accumulation of risk. This variability can result in significant deviations from the expected performance. Therefore, an estimate of variability (which is called <span class="hlt">design</span> risk in this study) together with the expected performance characteristic value (e.g. mean empty weight) is necessary for multidisciplinary optimization for a <span class="hlt">robust</span> <span class="hlt">design</span>. <span class="hlt">Robust</span> <span class="hlt">design</span> in this study is defined as a solution that minimizes variability subject to a constraint on mean performance characteristics. Even though multidisciplinary <span class="hlt">design</span> optimization has gained wide attention and applications, the treatment of uncertainties to quantify and analyze <span class="hlt">design</span> risk has received little attention. This research effort explores the dual response surface approach to quantify variability (risk) in critical performance characteristics (such as weight) during conceptual <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19910065106&hterms=comparative+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dcomparative%2Bdesign','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19910065106&hterms=comparative+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dcomparative%2Bdesign"><span><span class="hlt">Robust</span> Kalman filter <span class="hlt">design</span> for predictive wind shear detection</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stratton, Alexander D.; Stengel, Robert F.</p> <p>1991-01-01</p> <p>Severe, low-altitude wind shear is a threat to aviation safety. Airborne sensors under development measure the radial component of wind along a line directly in front of an aircraft. In this paper, optimal estimation theory is used to define a detection algorithm to warn of hazardous wind shear from these sensors. To achieve <span class="hlt">robustness</span>, a wind shear detection algorithm must distinguish threatening wind shear from less hazardous gustiness, despite variations in wind shear structure. This paper presents statistical analysis methods to refine wind shear detection algorithm <span class="hlt">robustness</span>. Computational methods predict the ability to warn of severe wind shear and avoid false warning. Comparative capability of the detection algorithm as a function of its <span class="hlt">design</span> parameters is determined, identifying <span class="hlt">designs</span> that provide <span class="hlt">robust</span> detection of severe wind shear.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940009145','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940009145"><span>Multidisciplinary <span class="hlt">Design</span> Techniques Applied to Conceptual Aerospace Vehicle <span class="hlt">Design</span>. Ph.D. Thesis Final Technical Report</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Olds, John Robert; Walberg, Gerald D.</p> <p>1993-01-01</p> <p>Multidisciplinary <span class="hlt">design</span> optimization (MDO) is an emerging discipline within aerospace engineering. Its goal is to bring structure and efficiency to the complex <span class="hlt">design</span> process associated with advanced aerospace launch vehicles. Aerospace vehicles generally require input from a variety of traditional aerospace disciplines - aerodynamics, structures, performance, etc. As such, traditional optimization methods cannot always be applied. Several multidisciplinary techniques and methods were proposed as potentially applicable to this class of <span class="hlt">design</span> problem. Among the candidate options are calculus-based (or gradient-based) optimization schemes and parametric schemes based on <span class="hlt">design</span> of experiments theory. A brief overview of several applicable multidisciplinary <span class="hlt">design</span> optimization methods is included. Methods from the calculus-based class and the parametric class are reviewed, but the research application reported focuses on methods from the parametric class. A vehicle of current interest was chosen as a test application for this research. The rocket-based combined-cycle (RBCC) single-stage-to-orbit (SSTO) launch vehicle combines elements of rocket and airbreathing propulsion in an attempt to produce an attractive option for launching medium sized payloads into low earth orbit. The RBCC SSTO presents a particularly difficult problem for traditional one-variable-at-a-time optimization methods because of the lack of an adequate experience base and the highly coupled nature of the <span class="hlt">design</span> variables. MDO, however, with it's structured approach to <span class="hlt">design</span>, is well suited to this problem. The result of the application of <span class="hlt">Taguchi</span> methods, central composite <span class="hlt">designs</span>, and response surface methods to the <span class="hlt">design</span> optimization of the RBCC SSTO are presented. Attention is given to the aspect of <span class="hlt">Taguchi</span> methods that attempts to locate a '<span class="hlt">robust</span>' <span class="hlt">design</span> - that is, a <span class="hlt">design</span> that is least sensitive to uncontrollable influences on the <span class="hlt">design</span>. Near-optimum minimum dry weight solutions are</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012JMEP...21.1978Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012JMEP...21.1978Y"><span>Optimization of Experimental Conditions of the Pulsed Current GTAW Parameters for Mechanical Properties of SDSS UNS S32760 Welds Based on the <span class="hlt">Taguchi</span> <span class="hlt">Design</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yousefieh, M.; Shamanian, M.; Saatchi, A.</p> <p>2012-09-01</p> <p><span class="hlt">Taguchi</span> <span class="hlt">design</span> method with L9 orthogonal array was implemented to optimize the pulsed current gas tungsten arc welding parameters for the hardness and the toughness of super duplex stainless steel (SDSS, UNS S32760) welds. In this regard, the hardness and the toughness were considered as performance characteristics. Pulse current, background current, % on time, and pulse frequency were chosen as main parameters. Each parameter was varied at three different levels. As a result of pooled analysis of variance, the pulse current is found to be the most significant factor for both the hardness and the toughness of SDSS welds by percentage contribution of 71.81 for hardness and 78.18 for toughness. The % on time (21.99%) and the background current (17.81%) had also the next most significant effect on the hardness and the toughness, respectively. The optimum conditions within the selected parameter values for hardness were found as the first level of pulse current (100 A), third level of background current (70 A), first level of % on time (40%), and first level of pulse frequency (1 Hz), while they were found as the second level of pulse current (120 A), second level of background current (60 A), second level of % on time (60%), and third level of pulse frequency (5 Hz) for toughness. The <span class="hlt">Taguchi</span> method was found to be a promising tool to obtain the optimum conditions for such studies. Finally, in order to verify experimental results, confirmation tests were carried out at optimum working conditions. Under these conditions, there were good agreements between the predicted and the experimental results for the both hardness and toughness.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28898905','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28898905"><span><span class="hlt">Taguchi</span> Experimental <span class="hlt">Design</span> for Optimization of Recombinant Human Growth Hormone Production in CHO Cell Lines and Comparing its Biological Activity with Prokaryotic Growth Hormone.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Aghili, Zahra Sadat; Zarkesh-Esfahani, Sayyed Hamid</p> <p>2018-02-01</p> <p>Growth hormone deficiency results in growth retardation in children and the GH deficiency syndrome in adults and they need to receive recombinant-GH in order to rectify the GH deficiency symptoms. Mammalian cells have become the favorite system for production of recombinant proteins for clinical application compared to prokaryotic systems because of their capability for appropriate protein folding, assembly, post-translational modification and proper signal. However, production level in mammalian cells is generally low compared to prokaryotic hosts. <span class="hlt">Taguchi</span> has established orthogonal arrays to describe a large number of experimental situations mainly to reduce experimental errors and to enhance the efficiency and reproducibility of laboratory experiments.In the present study, rhGH was produced in CHO cells and production of rhGH was assessed using Dot blotting, western blotting and Elisa assay. For optimization of rhGH production in CHO cells using <span class="hlt">Taguchi</span> method An M16 orthogonal experimental <span class="hlt">design</span> was used to investigate four different culture components. The biological activity of rhGH was assessed using LHRE-TK-Luciferase reporter gene system in HEK-293 and compared to the biological activity of prokaryotic rhGH.A maximal productivity of rhGH was reached in the conditions of 1%DMSO, 1%glycerol, 25 µM ZnSO 4 and 0 mM NaBu. Our findings indicate that control of culture conditions such as the addition of chemical components helps to develop an efficient large-scale and industrial process for the production of rhGH in CHO cells. Results of bioassay indicated that rhGH produced by CHO cells is able to induce GH-mediated intracellular cell signaling and showed higher bioactivity when compared to prokaryotic GH at the same concentrations. © Georg Thieme Verlag KG Stuttgart · New York.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ApSS..426..674V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ApSS..426..674V"><span><span class="hlt">Robust</span> superhydrophobic needle-like nanostructured ZnO surfaces prepared without post chemical-treatment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Velayi, Elmira; Norouzbeigi, Reza</p> <p>2017-12-01</p> <p><span class="hlt">Robust</span> superhydrophobic ZnO surfaces with micro/nano hybrid hierarchical structures were synthesized on the stainless steel mesh by a facile single-step chemical bath deposition (CBD) method without using further low surface energy materials. The <span class="hlt">Taguchi</span> L16 experimental <span class="hlt">design</span> was applied to evaluate the effects of reaction time, type and concentration of the additive, type of the chelating agent, and the molar ratio of the chelating agent to the initial zinc (II) ions. The prepared sample at the optimal conditions exhibited a sustainable and time-independent superhydrophobic behavior with the water contact angle (WCA) of 162.8° ± 2.5° and contact angle hysteresis (CAH) of 1.8° ± 0.5°. The XRD, SEM, TEM and FTIR analyses were used to characterize the prepared samples. Surface characterization using scanning electron microscopy (SEM) indicated accumulation of micro/nano branched ZnO needles on the substrate with the average diameters of ∼85 nm. After 20 abrasion cycles the optimum sample indicated an excellent mechanical <span class="hlt">robustness</span> via exposure to the pressure of 4.7 kPa. A suitable chemical resistance to the acidic and basic droplets with the pH range of 4 and 9 was observed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AIPC.1285..286L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AIPC.1285..286L"><span>Constrained Response Surface Optimisation and <span class="hlt">Taguchi</span> Methods for Precisely Atomising Spraying Process</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Luangpaiboon, P.; Suwankham, Y.; Homrossukon, S.</p> <p>2010-10-01</p> <p>This research presents a development of a <span class="hlt">design</span> of experiment technique for quality improvement in automotive manufacturing industrial. The quality of interest is the colour shade, one of the key feature and exterior appearance for the vehicles. With low percentage of first time quality, the manufacturer has spent a lot of cost for repaired works as well as the longer production time. To permanently dissolve such problem, the precisely spraying condition should be optimized. Therefore, this work will apply the full factorial <span class="hlt">design</span>, the multiple regression, the constrained response surface optimization methods or CRSOM, and <span class="hlt">Taguchi</span>'s method to investigate the significant factors and to determine the optimum factor level in order to improve the quality of paint shop. Firstly, 2κ full factorial was employed to study the effect of five factors including the paint flow rate at robot setting, the paint levelling agent, the paint pigment, the additive slow solvent, and non volatile solid at spraying of atomizing spraying machine. The response values of colour shade at 15 and 45 degrees were measured using spectrophotometer. Then the regression models of colour shade at both degrees were developed from the significant factors affecting each response. Consequently, both regression models were placed into the form of linear programming to maximize the colour shade subjected to 3 main factors including the pigment, the additive solvent and the flow rate. Finally, <span class="hlt">Taguchi</span>'s method was applied to determine the proper level of key variable factors to achieve the mean value target of colour shade. The factor of non volatile solid was found to be one more additional factor at this stage. Consequently, the proper level of all factors from both experiment <span class="hlt">design</span> methods were used to set a confirmation experiment. It was found that the colour shades, both visual at 15 and 45 angel of measurement degrees of spectrophotometer, were nearly closed to the target and the defective at</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4476202','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4476202"><span>An Efficient <span class="hlt">Taguchi</span> Approach for the Performance Optimization of Health, Safety, Environment and Ergonomics in Generation Companies</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Azadeh, Ali; Sheikhalishahi, Mohammad</p> <p>2014-01-01</p> <p>Background A unique framework for performance optimization of generation companies (GENCOs) based on health, safety, environment, and ergonomics (HSEE) indicators is presented. Methods To rank this sector of industry, the combination of data envelopment analysis (DEA), principal component analysis (PCA), and <span class="hlt">Taguchi</span> are used for all branches of GENCOs. These methods are applied in an integrated manner to measure the performance of GENCO. The preferred model between DEA, PCA, and <span class="hlt">Taguchi</span> is selected based on sensitivity analysis and maximum correlation between rankings. To achieve the stated objectives, noise is introduced into input data. Results The results show that <span class="hlt">Taguchi</span> outperforms other methods. Moreover, a comprehensive experiment is carried out to identify the most influential factor for ranking GENCOs. Conclusion The approach developed in this study could be used for continuous assessment and improvement of GENCO's performance in supplying energy with respect to HSEE factors. The results of such studies would help managers to have better understanding of weak and strong points in terms of HSEE factors. PMID:26106505</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4034650','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4034650"><span>Optimal <span class="hlt">Robust</span> Motion Controller <span class="hlt">Design</span> Using Multiobjective Genetic Algorithm</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Svečko, Rajko</p> <p>2014-01-01</p> <p>This paper describes the use of a multiobjective genetic algorithm for <span class="hlt">robust</span> motion controller <span class="hlt">design</span>. Motion controller structure is based on a disturbance observer in an RIC framework. The RIC approach is presented in the form with internal and external feedback loops, in which an internal disturbance rejection controller and an external performance controller must be synthesised. This paper involves novel objectives for <span class="hlt">robustness</span> and performance assessments for such an approach. Objective functions for the <span class="hlt">robustness</span> property of RIC are based on simple even polynomials with nonnegativity conditions. Regional pole placement method is presented with the aims of controllers' structures simplification and their additional arbitrary selection. Regional pole placement involves arbitrary selection of central polynomials for both loops, with additional admissible region of the optimized pole location. Polynomial deviation between selected and optimized polynomials is measured with derived performance objective functions. A multiobjective function is composed of different unrelated criteria such as <span class="hlt">robust</span> stability, controllers' stability, and time-performance indexes of closed loops. The <span class="hlt">design</span> of controllers and multiobjective optimization procedure involve a set of the objectives, which are optimized simultaneously with a genetic algorithm—differential evolution. PMID:24987749</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012JGeoS...2..234Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012JGeoS...2..234Y"><span>GPS baseline configuration <span class="hlt">design</span> based on <span class="hlt">robustness</span> analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yetkin, M.; Berber, M.</p> <p>2012-11-01</p> <p>The <span class="hlt">robustness</span> analysis results obtained from a Global Positioning System (GPS) network are dramatically influenced by the configuration<bold></bold>of the observed baselines. The selection of optimal GPS baselines may allow for a cost effective survey campaign and a sufficiently <span class="hlt">robust</span><bold></bold>network. Furthermore, using the approach described in this paper, the required number of sessions, the baselines to be observed, and the<bold></bold>significance levels for statistical testing and <span class="hlt">robustness</span> analysis can be determined even before the GPS campaign starts. In this study, we<bold></bold>propose a <span class="hlt">robustness</span> criterion for the optimal <span class="hlt">design</span> of geodetic networks, and present a very simple and efficient algorithm based on this<bold></bold>criterion for the selection of optimal GPS baselines. We also show the relationship between the number of sessions and the non-centrality<bold></bold>parameter. Finally, a numerical example is given to verify the efficacy of the proposed approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4721686','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4721686"><span>Optimisation in the <span class="hlt">Design</span> of Environmental Sensor Networks with <span class="hlt">Robustness</span> Consideration</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Budi, Setia; de Souza, Paulo; Timms, Greg; Malhotra, Vishv; Turner, Paul</p> <p>2015-01-01</p> <p>This work proposes the <span class="hlt">design</span> of Environmental Sensor Networks (ESN) through balancing <span class="hlt">robustness</span> and redundancy. An Evolutionary Algorithm (EA) is employed to find the optimal placement of sensor nodes in the Region of Interest (RoI). Data quality issues are introduced to simulate their impact on the performance of the ESN. Spatial Regression Test (SRT) is also utilised to promote <span class="hlt">robustness</span> in data quality of the <span class="hlt">designed</span> ESN. The proposed method provides high network representativeness (fit for purpose) with minimum sensor redundancy (cost), and ensures <span class="hlt">robustness</span> by enabling the network to continue to achieve its objectives when some sensors fail. PMID:26633392</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..184a2047H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..184a2047H"><span>Surface Roughness Optimization Using <span class="hlt">Taguchi</span> Method of High Speed End Milling For Hardened Steel D2</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hazza Faizi Al-Hazza, Muataz; Ibrahim, Nur Asmawiyah bt; Adesta, Erry T. Y.; Khan, Ahsan Ali; Abdullah Sidek, Atiah Bt.</p> <p>2017-03-01</p> <p>The main challenge for any manufacturer is to achieve higher quality of their final products with maintains minimum machining time. In this research final surface roughness analysed and optimized with maximum 0.3 mm flank wear length. The experiment was investigated the effect of cutting speed, feed rate and depth of cut on the final surface roughness using D2 as a work piece hardened to 52-56 HRC, and coated carbide as cutting tool with higher cutting speed 120-240 mm/min. The experiment has been conducted using L9 <span class="hlt">design</span> of <span class="hlt">Taguchi</span> collection. The results have been analysed using JMP software.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28389008','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28389008"><span><span class="hlt">Robust</span> fast controller <span class="hlt">design</span> via nonlinear fractional differential equations.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zhou, Xi; Wei, Yiheng; Liang, Shu; Wang, Yong</p> <p>2017-07-01</p> <p>A new method for linear system controller <span class="hlt">design</span> is proposed whereby the closed-loop system achieves both <span class="hlt">robustness</span> and fast response. The <span class="hlt">robustness</span> performance considered here means the damping ratio of closed-loop system can keep its desired value under system parameter perturbation, while the fast response, represented by rise time of system output, can be improved by tuning the controller parameter. We exploit techniques from both the nonlinear systems control and the fractional order systems control to derive a novel nonlinear fractional order controller. For theoretical analysis of the closed-loop system performance, two comparison theorems are developed for a class of fractional differential equations. Moreover, the rise time of the closed-loop system can be estimated, which facilitates our controller <span class="hlt">design</span> to satisfy the fast response performance and maintain the <span class="hlt">robustness</span>. Finally, numerical examples are given to illustrate the effectiveness of our methods. Copyright © 2017 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFM.H41B1298P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFM.H41B1298P"><span><span class="hlt">Robust</span> Bayesian Experimental <span class="hlt">Design</span> for Conceptual Model Discrimination</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pham, H. V.; Tsai, F. T. C.</p> <p>2015-12-01</p> <p>A <span class="hlt">robust</span> Bayesian optimal experimental <span class="hlt">design</span> under uncertainty is presented to provide firm information for model discrimination, given the least number of pumping wells and observation wells. Firm information is the maximum information of a system can be guaranteed from an experimental <span class="hlt">design</span>. The <span class="hlt">design</span> is based on the Box-Hill expected entropy decrease (EED) before and after the experiment <span class="hlt">design</span> and the Bayesian model averaging (BMA) framework. A max-min programming is introduced to choose the <span class="hlt">robust</span> <span class="hlt">design</span> that maximizes the minimal Box-Hill EED subject to that the highest expected posterior model probability satisfies a desired probability threshold. The EED is calculated by the Gauss-Hermite quadrature. The BMA method is used to predict future observations and to quantify future observation uncertainty arising from conceptual and parametric uncertainties in calculating EED. Monte Carlo approach is adopted to quantify the uncertainty in the posterior model probabilities. The optimal experimental <span class="hlt">design</span> is tested by a synthetic 5-layer anisotropic confined aquifer. Nine conceptual groundwater models are constructed due to uncertain geological architecture and boundary condition. High-performance computing is used to enumerate all possible <span class="hlt">design</span> solutions in order to identify the most plausible groundwater model. Results highlight the impacts of scedasticity in future observation data as well as uncertainty sources on potential pumping and observation locations.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_7 --> <div id="page_8" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="141"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014FrME....9....1Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014FrME....9....1Z"><span><span class="hlt">Robust</span> <span class="hlt">design</span> of configurations and parameters of adaptable products</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Jian; Chen, Yongliang; Xue, Deyi; Gu, Peihua</p> <p>2014-03-01</p> <p>An adaptable product can satisfy different customer requirements by changing its configuration and parameter values during the operation stage. <span class="hlt">Design</span> of adaptable products aims at reducing the environment impact through replacement of multiple different products with single adaptable ones. Due to the complex architecture, multiple functional requirements, and changes of product configurations and parameter values in operation, impact of uncertainties to the functional performance measures needs to be considered in <span class="hlt">design</span> of adaptable products. In this paper, a <span class="hlt">robust</span> <span class="hlt">design</span> approach is introduced to identify the optimal <span class="hlt">design</span> configuration and parameters of an adaptable product whose functional performance measures are the least sensitive to uncertainties. An adaptable product in this paper is modeled by both configurations and parameters. At the configuration level, methods to model different product configuration candidates in <span class="hlt">design</span> and different product configuration states in operation to satisfy <span class="hlt">design</span> requirements are introduced. At the parameter level, four types of product/operating parameters and relations among these parameters are discussed. A two-level optimization approach is developed to identify the optimal <span class="hlt">design</span> configuration and its parameter values of the adaptable product. A case study is implemented to illustrate the effectiveness of the newly developed <span class="hlt">robust</span> adaptable <span class="hlt">design</span> method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017Nanop...6..110W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017Nanop...6..110W"><span>Stochastic simulation and <span class="hlt">robust</span> <span class="hlt">design</span> optimization of integrated photonic filters</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Weng, Tsui-Wei; Melati, Daniele; Melloni, Andrea; Daniel, Luca</p> <p>2017-01-01</p> <p>Manufacturing variations are becoming an unavoidable issue in modern fabrication processes; therefore, it is crucial to be able to include stochastic uncertainties in the <span class="hlt">design</span> phase. In this paper, integrated photonic coupled ring resonator filters are considered as an example of significant interest. The sparsity structure in photonic circuits is exploited to construct a sparse combined generalized polynomial chaos model, which is then used to analyze related statistics and perform <span class="hlt">robust</span> <span class="hlt">design</span> optimization. Simulation results show that the optimized circuits are more <span class="hlt">robust</span> to fabrication process variations and achieve a reduction of 11%-35% in the mean square errors of the 3 dB bandwidth compared to unoptimized nominal <span class="hlt">designs</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1805e0003S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1805e0003S"><span><span class="hlt">Taguchi</span> optimization: Case study of gold recovery from amalgamation tailing by using froth flotation method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sudibyo, Aji, B. B.; Sumardi, S.; Mufakir, F. R.; Junaidi, A.; Nurjaman, F.; Karna, Aziza, Aulia</p> <p>2017-01-01</p> <p>Gold amalgamation process was widely used to treat gold ore. This process produces the tailing or amalgamation solid waste, which still contains gold at 8-9 ppm. Froth flotation is one of the promising methods to beneficiate gold from this tailing. However, this process requires optimal conditions which depends on the type of raw material. In this study, <span class="hlt">Taguchi</span> method was used to optimize the optimum conditions of the froth flotation process. The <span class="hlt">Taguchi</span> optimization shows that the gold recovery was strongly influenced by the particle size which is the best particle size at 150 mesh followed by the Potassium amyl xanthate concentration, pH and pine oil concentration at 1133.98, 4535.92 and 68.04 gr/ton amalgamation tailing, respectively.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940020486','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940020486"><span>Integrated <span class="hlt">design</span> and manufacturing for the high speed civil transport</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p></p> <p>1993-01-01</p> <p>In June 1992, Georgia Tech's School of Aerospace Engineering was awarded a NASA University Space Research Association (USRA) Advanced <span class="hlt">Design</span> Program (ADP) to address 'Integrated <span class="hlt">Design</span> and Manufacturing for the High Speed Civil Transport (HSCT)' in its graduate aerospace systems <span class="hlt">design</span> courses. This report summarizes the results of the five courses incorporated into the Georgia Tech's USRA ADP program. It covers AE8113: Introduction to Concurrent Engineering, AE4360: Introduction to CAE/CAD, AE4353: <span class="hlt">Design</span> for Life Cycle Cost, AE6351: Aerospace Systems <span class="hlt">Design</span> One, and AE6352: Aerospace Systems <span class="hlt">Design</span> Two. AE8113: Introduction to Concurrent Engineering was an introductory course addressing the basic principles of concurrent engineering (CE) or integrated product development (IPD). The <span class="hlt">design</span> of a total system was not the objective of this course. The goal was to understand and define the 'up-front' customer requirements, their decomposition, and determine the value objectives for a complex product, such as the high speed civil transport (HSCT). A generic CE methodology developed at Georgia Tech was used for this purpose. AE4353: <span class="hlt">Design</span> for Life Cycle Cost addressed the basic economic issues for an HSCT using a <span class="hlt">robust</span> <span class="hlt">design</span> technique, <span class="hlt">Taguchi</span>'s parameter <span class="hlt">design</span> optimization method (PDOM). An HSCT economic sensitivity assessment was conducted using a <span class="hlt">Taguchi</span> PDOM approach to address the <span class="hlt">robustness</span> of the basic HSCT <span class="hlt">design</span>. AE4360: Introduction to CAE/CAD permitted students to develop and utilize CAE/CAD/CAM knowledge and skills using CATIA and CADAM as the basic geometric tools. AE6351: Aerospace Systems <span class="hlt">Design</span> One focused on the conceptual <span class="hlt">design</span> refinement of a baseline HSCT configuration as defined by Boeing, Douglas, and NASA in their system studies. It required the use of NASA's synthesis codes FLOPS and ACSYNT. A criterion called the productivity index (P.I.) was used to evaluate disciplinary sensitivities and provide refinements of the baseline HSCT</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..MARP17009H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..MARP17009H"><span><span class="hlt">Robust</span> peptide bundles <span class="hlt">designed</span> computationally</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Haider, Michael; Zhang, Huixi Violet; Kiick, Kristi; Saven, Jeffery; Pochan, Darrin</p> <p></p> <p>Peptides are ideal candidates for the <span class="hlt">design</span> and controlled assembly of nanoscale materials due to their potential to assemble with atomistic precision as in biological systems. Unlike other work utilizing natural proteins and structural motifs, this effort is completely de novo in order to build arbitrary structures with desired size for the specific placement and separation of functional groups. We have successfully computationally <span class="hlt">designed</span> soluble, coiled coil, peptide, tetramer bundles which are <span class="hlt">robust</span> and stable. Using circular dichroism we demonstrated the thermal stability of these bundles as well as confirmed their alpha helical and coiled coil nature. The stability of these bundles arises from the computational <span class="hlt">design</span> of the coiled coil interior core residues. The coiled coil tetramer was confirmed to be the dominant species by analytical ultra-centrifugation sedimentation studies. We also established how these bundles behave in solution using small angle neutron scattering. The form factor of the bundles is well represented by a cylinder model and their behavior at high concentrations is modeled using a structure factor for aggregates of the cylinders. All of these experiments support our claim that the <span class="hlt">designed</span> coiled coil bundles were achieved in solution. NSF DMREF 1234161.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AIPC.1943b0051S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AIPC.1943b0051S"><span>Experimental investigation and optimization of welding process parameters for various steel grades using NN tool and <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Soni, Sourabh Kumar; Thomas, Benedict</p> <p>2018-04-01</p> <p>The term "weldability" has been used to describe a wide variety of characteristics when a material is subjected to welding. In our analysis we perform experimental investigation to estimate the tensile strength of welded joint strength and then optimization of welding process parameters by using <span class="hlt">taguchi</span> method and Artificial Neural Network (ANN) tool in MINITAB and MATLAB software respectively. The study reveals the influence on weldability of steel by varying composition of steel by mechanical characterization. At first we prepare the samples of different grades of steel (EN8, EN 19, EN 24). The samples were welded together by metal inert gas welding process and then tensile testing on Universal testing machine (UTM) was conducted for the same to evaluate the tensile strength of the welded steel specimens. Further comparative study was performed to find the effects of welding parameter on quality of weld strength by employing <span class="hlt">Taguchi</span> method and Neural Network tool. Finally we concluded that <span class="hlt">taguchi</span> method and Neural Network Tool is much efficient technique for optimization.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20070018832','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20070018832"><span><span class="hlt">Robust</span> <span class="hlt">Design</span> Optimization via Failure Domain Bounding</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crespo, Luis G.; Kenny, Sean P.; Giesy, Daniel P.</p> <p>2007-01-01</p> <p>This paper extends and applies the strategies recently developed by the authors for handling constraints under uncertainty to <span class="hlt">robust</span> <span class="hlt">design</span> optimization. For the scope of this paper, <span class="hlt">robust</span> optimization is a methodology aimed at problems for which some parameters are uncertain and are only known to belong to some uncertainty set. This set can be described by either a deterministic or a probabilistic model. In the methodology developed herein, optimization-based strategies are used to bound the constraint violation region using hyper-spheres and hyper-rectangles. By comparing the resulting bounding sets with any given uncertainty model, it can be determined whether the constraints are satisfied for all members of the uncertainty model (i.e., constraints are feasible) or not (i.e., constraints are infeasible). If constraints are infeasible and a probabilistic uncertainty model is available, upper bounds to the probability of constraint violation can be efficiently calculated. The tools developed enable approximating not only the set of <span class="hlt">designs</span> that make the constraints feasible but also, when required, the set of <span class="hlt">designs</span> for which the probability of constraint violation is below a prescribed admissible value. When constraint feasibility is possible, several <span class="hlt">design</span> criteria can be used to shape the uncertainty model of performance metrics of interest. Worst-case, least-second-moment, and reliability-based <span class="hlt">design</span> criteria are considered herein. Since the problem formulation is generic and the tools derived only require standard optimization algorithms for their implementation, these strategies are easily applicable to a broad range of engineering problems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820004207','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820004207"><span>Computational methods of <span class="hlt">robust</span> controller <span class="hlt">design</span> for aerodynamic flutter suppression</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anderson, L. R.</p> <p>1981-01-01</p> <p>The development of Riccati iteration, a tool for the <span class="hlt">design</span> and analysis of linear control systems is examined. First, Riccati iteration is applied to the problem of pole placement and order reduction in two-time scale control systems. Order reduction, yielding a good approximation to the original system, is demonstrated using a 16th order linear model of a turbofan engine. Next, a numerical method for solving the Riccati equation is presented and demonstrated for a set of eighth order random examples. A literature review of <span class="hlt">robust</span> controller <span class="hlt">design</span> methods follows which includes a number of methods for reducing the trajectory and performance index sensitivity in linear regulators. Lastly, <span class="hlt">robust</span> controller <span class="hlt">design</span> for large parameter variations is discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19810053428&hterms=transmission+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtransmission%2Bdesign','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19810053428&hterms=transmission+design&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtransmission%2Bdesign"><span>Penetrating transmission zeros in the <span class="hlt">design</span> of <span class="hlt">robust</span> servomechanism systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wang, S. H.; Davison, E. J.</p> <p>1981-01-01</p> <p>In the <span class="hlt">design</span> of a <span class="hlt">robust</span> servomechanism system, it is well known that the system cannot track a reference signal whose frequency coincides with the transmission zeros of the system. This paper proposes a new <span class="hlt">design</span> method for overcoming this difficulty. The controller to be used employs a sampler and holding device with exponential decay. It is shown that the transmission zeros of the discretized system can be shifted by changing the rate of the exponential decay of the holding device. Thus, it is possible to <span class="hlt">design</span> a <span class="hlt">robust</span> controller for the discretized system to track any reference signal of given frequency, even if the given frequency coincides with the transmission zeros of the original continuous-time system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25295306','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25295306"><span>SVM-RFE based feature selection and <span class="hlt">Taguchi</span> parameters optimization for multiclass SVM classifier.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Huang, Mei-Ling; Hung, Yung-Hsiang; Lee, W M; Li, R K; Jiang, Bo-Ru</p> <p>2014-01-01</p> <p>Recently, support vector machine (SVM) has excellent performance on classification and prediction and is widely used on disease diagnosis or medical assistance. However, SVM only functions well on two-group classification problems. This study combines feature selection and SVM recursive feature elimination (SVM-RFE) to investigate the classification accuracy of multiclass problems for Dermatology and Zoo databases. Dermatology dataset contains 33 feature variables, 1 class variable, and 366 testing instances; and the Zoo dataset contains 16 feature variables, 1 class variable, and 101 testing instances. The feature variables in the two datasets were sorted in descending order by explanatory power, and different feature sets were selected by SVM-RFE to explore classification accuracy. Meanwhile, <span class="hlt">Taguchi</span> method was jointly combined with SVM classifier in order to optimize parameters C and γ to increase classification accuracy for multiclass classification. The experimental results show that the classification accuracy can be more than 95% after SVM-RFE feature selection and <span class="hlt">Taguchi</span> parameter optimization for Dermatology and Zoo databases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4175386','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4175386"><span>SVM-RFE Based Feature Selection and <span class="hlt">Taguchi</span> Parameters Optimization for Multiclass SVM Classifier</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Huang, Mei-Ling; Hung, Yung-Hsiang; Lee, W. M.; Li, R. K.; Jiang, Bo-Ru</p> <p>2014-01-01</p> <p>Recently, support vector machine (SVM) has excellent performance on classification and prediction and is widely used on disease diagnosis or medical assistance. However, SVM only functions well on two-group classification problems. This study combines feature selection and SVM recursive feature elimination (SVM-RFE) to investigate the classification accuracy of multiclass problems for Dermatology and Zoo databases. Dermatology dataset contains 33 feature variables, 1 class variable, and 366 testing instances; and the Zoo dataset contains 16 feature variables, 1 class variable, and 101 testing instances. The feature variables in the two datasets were sorted in descending order by explanatory power, and different feature sets were selected by SVM-RFE to explore classification accuracy. Meanwhile, <span class="hlt">Taguchi</span> method was jointly combined with SVM classifier in order to optimize parameters C and γ to increase classification accuracy for multiclass classification. The experimental results show that the classification accuracy can be more than 95% after SVM-RFE feature selection and <span class="hlt">Taguchi</span> parameter optimization for Dermatology and Zoo databases. PMID:25295306</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JIEIC..99...45S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JIEIC..99...45S"><span>Modelling the Cast Component Weight in Hot Chamber Die Casting using Combined <span class="hlt">Taguchi</span> and Buckingham's π Approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Singh, Rupinder</p> <p>2018-02-01</p> <p>Hot chamber (HC) die casting process is one of the most widely used commercial processes for the casting of low temperature metals and alloys. This process gives near-net shape product with high dimensional accuracy. However in actual field environment the best settings of input parameters is often conflicting as the shape and size of the casting changes and one have to trade off among various output parameters like hardness, dimensional accuracy, casting defects, microstructure etc. So for online inspection of the cast components properties (without affecting the production line) the weight measurement has been established as one of the cost effective method (as the difference in weight of sound and unsound casting reflects the possible casting defects) in field environment. In the present work at first stage the effect of three input process parameters (namely: pressure at 2nd phase in HC die casting; metal pouring temperature and die opening time) has been studied for optimizing the cast component weight `W' as output parameter in form of macro model based upon <span class="hlt">Taguchi</span> L9 OA. After this Buckingham's π approach has been applied on <span class="hlt">Taguchi</span> based macro model for the development of micro model. This study highlights the <span class="hlt">Taguchi</span>-Buckingham based combined approach as a case study (for conversion of macro model into micro model) by identification of optimum levels of input parameters (based on <span class="hlt">Taguchi</span> approach) and development of mathematical model (based on Buckingham's π approach). Finally developed mathematical model can be used for predicting W in HC die casting process with more flexibility. The results of study highlights second degree polynomial equation for predicting cast component weight in HC die casting and suggest that pressure at 2nd stage is one of the most contributing factors for controlling the casting defect/weight of casting.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993STIN...9322458R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993STIN...9322458R"><span><span class="hlt">Robustness</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ryan, R.</p> <p>1993-03-01</p> <p><span class="hlt">Robustness</span> is a buzz word common to all newly proposed space systems <span class="hlt">design</span> as well as many new commercial products. The image that one conjures up when the word appears is a 'Paul Bunyon' (lumberjack <span class="hlt">design</span>), strong and hearty; healthy with margins in all aspects of the <span class="hlt">design</span>. In actuality, <span class="hlt">robustness</span> is much broader in scope than margins, including such factors as simplicity, redundancy, desensitization to parameter variations, control of parameter variations (environments flucation), and operational approaches. These must be traded with concepts, materials, and fabrication approaches against the criteria of performance, cost, and reliability. This includes manufacturing, assembly, processing, checkout, and operations. The <span class="hlt">design</span> engineer or project chief is faced with finding ways and means to inculcate <span class="hlt">robustness</span> into an operational <span class="hlt">design</span>. First, however, be sure he understands the definition and goals of <span class="hlt">robustness</span>. This paper will deal with these issues as well as the need for the requirement for <span class="hlt">robustness</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930013269','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930013269"><span><span class="hlt">Robustness</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ryan, R.</p> <p>1993-01-01</p> <p><span class="hlt">Robustness</span> is a buzz word common to all newly proposed space systems <span class="hlt">design</span> as well as many new commercial products. The image that one conjures up when the word appears is a 'Paul Bunyon' (lumberjack <span class="hlt">design</span>), strong and hearty; healthy with margins in all aspects of the <span class="hlt">design</span>. In actuality, <span class="hlt">robustness</span> is much broader in scope than margins, including such factors as simplicity, redundancy, desensitization to parameter variations, control of parameter variations (environments flucation), and operational approaches. These must be traded with concepts, materials, and fabrication approaches against the criteria of performance, cost, and reliability. This includes manufacturing, assembly, processing, checkout, and operations. The <span class="hlt">design</span> engineer or project chief is faced with finding ways and means to inculcate <span class="hlt">robustness</span> into an operational <span class="hlt">design</span>. First, however, be sure he understands the definition and goals of <span class="hlt">robustness</span>. This paper will deal with these issues as well as the need for the requirement for <span class="hlt">robustness</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ApSS..422..787M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ApSS..422..787M"><span>Fabrication of flower-like micro/nano dual scale structured copper oxide surfaces: Optimization of self-cleaning properties via <span class="hlt">Taguchi</span> <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Moosavi, Saeideh Sadat; Norouzbeigi, Reza; Velayi, Elmira</p> <p>2017-11-01</p> <p>In the present work, copper oxide superhydrophobic surface is fabricated on a copper foil via the chemical bath deposition (CBD) method. The effects of some influential factors such as initial concentrations of Cu (II) ions and the surface energy modifier, solution pH, reaction and modification steps time on the wettability property of copper oxide surface were evaluated using <span class="hlt">Taguchi</span> L16 experimental <span class="hlt">design</span>. Results showed that the initial concentration of Cu (II) has the most significant impact on the water contact angle and wettability characteristics. The XRD, SEM, AFM and FTIR analyses were used to characterize the copper oxide surfaces. The Water contact angle (WCA) and contact angle hysteresis (CAH) were also measured. The SEM results indicated the formation of a flower-like micro/nano dual-scale structure of copper oxide on the substrate. This structure composed of numerous nano-petals with a thickness of about 50 nm. As a result, a copper oxide hierarchical surface with WCA of 168.4°± 3.5° and CAH of 2.73° exhibited the best superhydrophobicity under proposed optimum condition. This result has been obtained just by 10 min hydrolysis reaction. Besides, this surface showed a good stability under acidic and saline conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15812798','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15812798"><span>Anaerobic treatment of complex chemical wastewater in a sequencing batch biofilm reactor: process optimization and evaluation of factor interactions using the <span class="hlt">Taguchi</span> dynamic DOE methodology.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Venkata Mohan, S; Chandrasekhara Rao, N; Krishna Prasad, K; Murali Krishna, P; Sreenivas Rao, R; Sarma, P N</p> <p>2005-06-20</p> <p>The <span class="hlt">Taguchi</span> <span class="hlt">robust</span> experimental <span class="hlt">design</span> (DOE) methodology has been applied on a dynamic anaerobic process treating complex wastewater by an anaerobic sequencing batch biofilm reactor (AnSBBR). For optimizing the process as well as to evaluate the influence of different factors on the process, the uncontrollable (noise) factors have been considered. The <span class="hlt">Taguchi</span> methodology adopting dynamic approach is the first of its kind for studying anaerobic process evaluation and process optimization. The <span class="hlt">designed</span> experimental methodology consisted of four phases--planning, conducting, analysis, and validation connected sequence-wise to achieve the overall optimization. In the experimental <span class="hlt">design</span>, five controllable factors, i.e., organic loading rate (OLR), inlet pH, biodegradability (BOD/COD ratio), temperature, and sulfate concentration, along with the two uncontrollable (noise) factors, volatile fatty acids (VFA) and alkalinity at two levels were considered for optimization of the anae robic system. Thirty-two anaerobic experiments were conducted with a different combination of factors and the results obtained in terms of substrate degradation rates were processed in Qualitek-4 software to study the main effect of individual factors, interaction between the individual factors, and signal-to-noise (S/N) ratio analysis. Attempts were also made to achieve optimum conditions. Studies on the influence of individual factors on process performance revealed the intensive effect of OLR. In multiple factor interaction studies, biodegradability with other factors, such as temperature, pH, and sulfate have shown maximum influence over the process performance. The optimum conditions for the efficient performance of the anaerobic system in treating complex wastewater by considering dynamic (noise) factors obtained are higher organic loading rate of 3.5 Kg COD/m3 day, neutral pH with high biodegradability (BOD/COD ratio of 0.5), along with mesophilic temperature range (40 degrees C), and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhyC..550...57A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhyC..550...57A"><span>Optimization of radial-type superconducting magnetic bearing using the <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ai, Liwang; Zhang, Guomin; Li, Wanjie; Liu, Guole; Liu, Qi</p> <p>2018-07-01</p> <p>It is important and complicated to model and optimize the levitation behavior of superconducting magnetic bearing (SMB). That is due to the nonlinear constitutive relationships of superconductor and ferromagnetic materials, the relative movement between the superconducting stator and PM rotor, and the multi-parameter (e.g., air-gap, critical current density, and remanent flux density, etc.) affecting the levitation behavior. In this paper, we present a theoretical calculation and optimization method of the levitation behavior for radial-type SMB. A simplified model of levitation force calculation is established using 2D finite element method with H-formulation. In the model, the boundary condition of superconducting stator is imposed by harmonic series expressions to describe the traveling magnetic field generated by the moving PM rotor. Also, experimental measurements of the levitation force are performed and validate the model method. A statistical method called <span class="hlt">Taguchi</span> method is adopted to carry out an optimization of load capacity for SMB. Then the factor effects of six optimization parameters on the target characteristics are discussed and the optimum parameters combination is determined finally. The results show that the levitation behavior of SMB is greatly improved and the <span class="hlt">Taguchi</span> method is suitable for optimizing the SMB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19780034555&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19780034555&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda"><span><span class="hlt">Robustness</span> of linear quadratic state feedback <span class="hlt">designs</span> in the presence of system uncertainty. [applied to STOL autopilot <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Patel, R. V.; Toda, M.; Sridhar, B.</p> <p>1977-01-01</p> <p>In connection with difficulties concerning an accurate mathematical representation of a linear quadratic state feedback (LQSF) system, it is often necessary to investigate the <span class="hlt">robustness</span> (stability) of an LQSF <span class="hlt">design</span> in the presence of system uncertainty and obtain some quantitative measure of the perturbations which such a <span class="hlt">design</span> can tolerate. A study is conducted concerning the problem of expressing the <span class="hlt">robustness</span> property of an LQSF <span class="hlt">design</span> quantitatively in terms of bounds on the perturbations (modeling errors or parameter variations) in the system matrices. Bounds are obtained for the general case of nonlinear, time-varying perturbations. It is pointed out that most of the presented results are readily applicable to practical situations for which a <span class="hlt">designer</span> has estimates of the bounds on the system parameter perturbations. Relations are provided which help the <span class="hlt">designer</span> to select appropriate weighting matrices in the quadratic performance index to attain a <span class="hlt">robust</span> <span class="hlt">design</span>. The developed results are employed in the <span class="hlt">design</span> of an autopilot logic for the flare maneuver of the Augmentor Wing Jet STOL Research Aircraft.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25376052','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25376052"><span><span class="hlt">Robust</span> Frequency-Domain Constrained Feedback <span class="hlt">Design</span> via a Two-Stage Heuristic Approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Li, Xianwei; Gao, Huijun</p> <p>2015-10-01</p> <p>Based on a two-stage heuristic method, this paper is concerned with the <span class="hlt">design</span> of <span class="hlt">robust</span> feedback controllers with restricted frequency-domain specifications (RFDSs) for uncertain linear discrete-time systems. Polytopic uncertainties are assumed to enter all the system matrices, while RFDSs are motivated by the fact that practical <span class="hlt">design</span> specifications are often described in restricted finite frequency ranges. Dilated multipliers are first introduced to relax the generalized Kalman-Yakubovich-Popov lemma for output feedback controller synthesis and <span class="hlt">robust</span> performance analysis. Then a two-stage approach to output feedback controller synthesis is proposed: at the first stage, a <span class="hlt">robust</span> full-information (FI) controller is <span class="hlt">designed</span>, which is used to construct a required output feedback controller at the second stage. To improve the solvability of the synthesis method, heuristic iterative algorithms are further formulated for exploring the feedback gain and optimizing the initial FI controller at the individual stage. The effectiveness of the proposed <span class="hlt">design</span> method is finally demonstrated by the application to active control of suspension systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950010059','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950010059"><span>Matlab as a <span class="hlt">robust</span> control <span class="hlt">design</span> tool</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gregory, Irene M.</p> <p>1994-01-01</p> <p>This presentation introduces Matlab as a tool used in flight control research. The example used to illustrate some of the capabilities of this software is a <span class="hlt">robust</span> controller <span class="hlt">designed</span> for a single stage to orbit air breathing vehicles's ascent to orbit. The global requirements of the controller are to stabilize the vehicle and follow a trajectory in the presence of atmospheric disturbances and strong dynamic coupling between airframe and propulsion.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_8 --> <div id="page_9" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="161"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010IEITC..91.3351M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010IEITC..91.3351M"><span><span class="hlt">Robust</span> Transceiver <span class="hlt">Design</span> for Multiuser MIMO Downlink with Channel Uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Miao, Wei; Li, Yunzhou; Chen, Xiang; Zhou, Shidong; Wang, Jing</p> <p></p> <p>This letter addresses the problem of <span class="hlt">robust</span> transceiver <span class="hlt">design</span> for the multiuser multiple-input-multiple-output (MIMO) downlink where the channel state information at the base station (BS) is imperfect. A stochastic approach which minimizes the expectation of the total mean square error (MSE) of the downlink conditioned on the channel estimates under a total transmit power constraint is adopted. The iterative algorithm reported in [2] is improved to handle the proposed <span class="hlt">robust</span> optimization problem. Simulation results show that our proposed <span class="hlt">robust</span> scheme effectively reduces the performance loss due to channel uncertainties and outperforms existing methods, especially when the channel errors of the users are different.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011AIPC.1383..927X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011AIPC.1383..927X"><span><span class="hlt">Robust</span> <span class="hlt">Design</span> of Sheet Metal Forming Process Based on Kriging Metamodel</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xie, Yanmin</p> <p>2011-08-01</p> <p>Nowadays, sheet metal forming processes <span class="hlt">design</span> is not a trivial task due to the complex issues to be taken into account (conflicting <span class="hlt">design</span> goals, complex shapes forming and so on). Optimization methods have also been widely applied in sheet metal forming. Therefore, proper <span class="hlt">design</span> methods to reduce time and costs have to be developed mostly based on computer aided procedures. At the same time, the existence of variations during manufacturing processes significantly may influence final product quality, rendering non-<span class="hlt">robust</span> optimal solutions. In this paper, a small size of <span class="hlt">design</span> of experiments is conducted to investigate how a stochastic behavior of noise factors affects drawing quality. The finite element software (LS_DYNA) is used to simulate the complex sheet metal stamping processes. The Kriging metamodel is adopted to map the relation between input process parameters and part quality. <span class="hlt">Robust</span> <span class="hlt">design</span> models for sheet metal forming process integrate adaptive importance sampling with Kriging model, in order to minimize impact of the variations and achieve reliable process parameters. In the adaptive sample, an improved criterion is used to provide direction in which additional training samples can be added to better the Kriging model. Nonlinear functions as test functions and a square stamping example (NUMISHEET'93) are employed to verify the proposed method. Final results indicate application feasibility of the aforesaid method proposed for multi-response <span class="hlt">robust</span> <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JIEIC..98..119S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JIEIC..98..119S"><span>Parametric Optimization of Wire Electrical Discharge Machining of Powder Metallurgical Cold Worked Tool Steel using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sudhakara, Dara; Prasanthi, Guvvala</p> <p>2017-04-01</p> <p>Wire Cut EDM is an unconventional machining process used to build components of complex shape. The current work mainly deals with optimization of surface roughness while machining P/M CW TOOL STEEL by Wire cut EDM using <span class="hlt">Taguchi</span> method. The process parameters of the Wire Cut EDM is ON, OFF, IP, SV, WT, and WP. L27 OA is used for to <span class="hlt">design</span> of the experiments for conducting experimentation. In order to find out the effecting parameters on the surface roughness, ANOVA analysis is engaged. The optimum levels for getting minimum surface roughness is ON = 108 µs, OFF = 63 µs, IP = 11 A, SV = 68 V and WT = 8 g.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..203a2016R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..203a2016R"><span>Optimization of bone drilling parameters using <span class="hlt">Taguchi</span> method based on finite element analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rosidi, Ayip; Lenggo Ginta, Turnad; Rani, Ahmad Majdi Bin Abdul</p> <p>2017-05-01</p> <p>Thermal necrosis results fracture problems and implant failure if temperature exceeds 47 °C for one minute during bone drilling. To solve this problem, this work studied a new thermal model by using three drilling parameters: drill diameter, feed rate and spindle speed. Effects of those parameters to heat generation were studied. The drill diameters were 4 mm, 6 mm and 6 mm; the feed rates were 80 mm/min, 100 mm/min and 120 mm/min whereas the spindle speeds were 400 rpm, 500 rpm and 600 rpm then an optimization was done by <span class="hlt">Taguchi</span> method to which combination parameter can be used to prevent thermal necrosis during bone drilling. The results showed that all the combination of parameters produce confidence results which were below 47 °C and finite element analysis combined with <span class="hlt">Taguchi</span> method can be used for predicting temperature generation and optimizing bone drilling parameters prior to clinical bone drilling. All of the combination parameters can be used for surgeon to achieve sustainable orthopaedic surgery.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.908a2041J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.908a2041J"><span>Investigating the effects of PDC cutters geometry on ROP using the <span class="hlt">Taguchi</span> technique</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jamaludin, A. A.; Mehat, N. M.; Kamaruddin, S.</p> <p>2017-10-01</p> <p>At times, the polycrystalline diamond compact (PDC) bit’s performance dropped and affects the rate of penetration (ROP). The objective of this project is to investigate the effect of PDC cutter geometry and optimize them. An intensive study in cutter geometry would further enhance the ROP performance. The relatively extended analysis was carried out and four significant geometry factors have been identified that directly improved the ROP. Cutter size, back rake angle, side rake angle and chamfer angle are the stated geometry factors. An appropriate optimization technique that effectively controls all influential geometry factors during cutters manufacturing is introduced and adopted in this project. By adopting L9 <span class="hlt">Taguchi</span> OA, simulation experiment is conducted by using explicit dynamics finite element analysis. Through a structure <span class="hlt">Taguchi</span> analysis, ANOVA confirms that the most significant geometry to improve ROP is cutter size (99.16% percentage contribution). The optimized cutter is expected to drill with high ROP that can reduce the rig time, which in its turn, may reduce the total drilling cost.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4914944','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4914944"><span>A Statistical Approach Reveals <span class="hlt">Designs</span> for the Most <span class="hlt">Robust</span> Stochastic Gene Oscillators</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2016-01-01</p> <p>The engineering of transcriptional networks presents many challenges due to the inherent uncertainty in the system structure, changing cellular context, and stochasticity in the governing dynamics. One approach to address these problems is to <span class="hlt">design</span> and build systems that can function across a range of conditions; that is they are <span class="hlt">robust</span> to uncertainty in their constituent components. Here we examine the parametric <span class="hlt">robustness</span> landscape of transcriptional oscillators, which underlie many important processes such as circadian rhythms and the cell cycle, plus also serve as a model for the engineering of complex and emergent phenomena. The central questions that we address are: Can we build genetic oscillators that are more <span class="hlt">robust</span> than those already constructed? Can we make genetic oscillators arbitrarily <span class="hlt">robust</span>? These questions are technically challenging due to the large model and parameter spaces that must be efficiently explored. Here we use a measure of <span class="hlt">robustness</span> that coincides with the Bayesian model evidence, combined with an efficient Monte Carlo method to traverse model space and concentrate on regions of high <span class="hlt">robustness</span>, which enables the accurate evaluation of the relative <span class="hlt">robustness</span> of gene network models governed by stochastic dynamics. We report the most <span class="hlt">robust</span> two and three gene oscillator systems, plus examine how the number of interactions, the presence of autoregulation, and degradation of mRNA and protein affects the frequency, amplitude, and <span class="hlt">robustness</span> of transcriptional oscillators. We also find that there is a limit to parametric <span class="hlt">robustness</span>, beyond which there is nothing to be gained by adding additional feedback. Importantly, we provide predictions on new oscillator systems that can be constructed to verify the theory and advance <span class="hlt">design</span> and modeling approaches to systems and synthetic biology. PMID:26835539</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030065878','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030065878"><span>Reliability Assessment of a <span class="hlt">Robust</span> <span class="hlt">Design</span> Under Uncertainty for a 3-D Flexible Wing</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gumbert, Clyde R.; Hou, Gene J. -W.; Newman, Perry A.</p> <p>2003-01-01</p> <p>The paper presents reliability assessment results for the <span class="hlt">robust</span> <span class="hlt">designs</span> under uncertainty of a 3-D flexible wing previously reported by the authors. Reliability assessments (additional optimization problems) of the active constraints at the various probabilistic <span class="hlt">robust</span> <span class="hlt">design</span> points are obtained and compared with the constraint values or target constraint probabilities specified in the <span class="hlt">robust</span> <span class="hlt">design</span>. In addition, reliability-based sensitivity derivatives with respect to <span class="hlt">design</span> variable mean values are also obtained and shown to agree with finite difference values. These derivatives allow one to perform reliability based <span class="hlt">design</span> without having to obtain second-order sensitivity derivatives. However, an inner-loop optimization problem must be solved for each active constraint to find the most probable point on that constraint failure surface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2003SPIE.5020..215R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2003SPIE.5020..215R"><span>Optimized selection of benchmark test parameters for image watermark algorithms based on <span class="hlt">Taguchi</span> methods and corresponding influence on <span class="hlt">design</span> decisions for real-world applications</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rodriguez, Tony F.; Cushman, David A.</p> <p>2003-06-01</p> <p>With the growing commercialization of watermarking techniques in various application scenarios it has become increasingly important to quantify the performance of watermarking products. The quantification of relative merits of various products is not only essential in enabling further adoption of the technology by society as a whole, but will also drive the industry to develop testing plans/methodologies to ensure quality and minimize cost (to both vendors & customers.) While the research community understands the theoretical need for a publicly available benchmarking system to quantify performance, there has been less discussion on the practical application of these systems. By providing a standard set of acceptance criteria, benchmarking systems can dramatically increase the quality of a particular watermarking solution, validating the product performances if they are used efficiently and frequently during the <span class="hlt">design</span> process. In this paper we describe how to leverage specific <span class="hlt">design</span> of experiments techniques to increase the quality of a watermarking scheme, to be used with the benchmark tools being developed by the Ad-Hoc Watermark Verification Group. A <span class="hlt">Taguchi</span> Loss Function is proposed for an application and orthogonal arrays used to isolate optimal levels for a multi-factor experimental situation. Finally, the results are generalized to a population of cover works and validated through an exhaustive test.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA524282','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA524282"><span>A <span class="hlt">Design</span> Tool for <span class="hlt">Robust</span> Composite Structures</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2010-06-01</p> <p>a a UNIVERSITY OF ^?CAiVI BRIDGE FINAL REPORT A <span class="hlt">Design</span> Tool for <span class="hlt">Robust</span> Composite Structures Frank Zok Materials Department University of ...organic fibers, especially Dyneema®. The principal objectives of the present study were to ascertain the fundamental mechanical properties of Dyneema...composites increases by a factor of 2 and the ductility by almost a factor of 3 over the strain rate range 10-3 s-1 to 104 s- 1. One consequence is</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1991gnc..conf.1059D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1991gnc..conf.1059D"><span><span class="hlt">Robust</span> flight <span class="hlt">design</span> for an advanced launch system vehicle</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dhand, Sanjeev K.; Wong, Kelvin K.</p> <p></p> <p>Current launch vehicle trajectory <span class="hlt">design</span> philosophies are generally based on maximizing payload capability. This approach results in an expensive trajectory <span class="hlt">design</span> process for each mission. Two concepts of <span class="hlt">robust</span> flight <span class="hlt">design</span> have been developed to significantly reduce this cost: Standardized Trajectories and Command Multiplier Steering (CMS). These concepts were analyzed for an Advanced Launch System (ALS) vehicle, although their applicability is not restricted to any particular vehicle. Preliminary analysis has demonstrated the feasibility of these concepts at minimal loss in payload capability.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930042435&hterms=SANJAY&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DSANJAY','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930042435&hterms=SANJAY&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3DSANJAY"><span><span class="hlt">Robust</span> integrated flight/propulsion control <span class="hlt">design</span> for a STOVL aircraft using H-infinity control <span class="hlt">design</span> techniques</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Garg, Sanjay</p> <p>1993-01-01</p> <p>Results are presented from an application of H-infinity control <span class="hlt">design</span> methodology to a centralized integrated flight/propulsion control (IFPC) system <span class="hlt">design</span> for a supersonic STOVL fighter aircraft in transition flight. The emphasis is on formulating the H-infinity optimal control synthesis problem such that the critical requirements for the flight and propulsion systems are adequately reflected within the linear, centralized control problem formulation and the resulting controller provides <span class="hlt">robustness</span> to modeling uncertainties and model parameter variations with flight condition. Detailed evaluation results are presented for a reduced order controller obtained from the improved H-infinity control <span class="hlt">design</span> showing that the control <span class="hlt">design</span> meets the specified nominal performance objective as well as provides stability <span class="hlt">robustness</span> for variations in plant system dynamics with changes in aircraft trim speed within the transition flight envelope.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920072575&hterms=jury&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Djury','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920072575&hterms=jury&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Djury"><span>Aircraft ride quality controller <span class="hlt">design</span> using new <span class="hlt">robust</span> root clustering theory for linear uncertain systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yedavalli, R. K.</p> <p>1992-01-01</p> <p>The aspect of controller <span class="hlt">design</span> for improving the ride quality of aircraft in terms of damping ratio and natural frequency specifications on the short period dynamics is addressed. The controller is <span class="hlt">designed</span> to be <span class="hlt">robust</span> with respect to uncertainties in the real parameters of the control <span class="hlt">design</span> model such as uncertainties in the dimensional stability derivatives, imperfections in actuator/sensor locations and possibly variations in flight conditions, etc. The <span class="hlt">design</span> is based on a new <span class="hlt">robust</span> root clustering theory developed by the author by extending the nominal root clustering theory of Gutman and Jury to perturbed matrices. The proposed methodology allows to get an explicit relationship between the parameters of the root clustering region and the uncertainty radius of the parameter space. The current literature available for <span class="hlt">robust</span> stability becomes a special case of this unified theory. The bounds derived on the parameter perturbation for <span class="hlt">robust</span> root clustering are then used in selecting the <span class="hlt">robust</span> controller.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19964418','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19964418"><span>A preferential <span class="hlt">design</span> approach for energy-efficient and <span class="hlt">robust</span> implantable neural signal processing hardware.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Narasimhan, Seetharam; Chiel, Hillel J; Bhunia, Swarup</p> <p>2009-01-01</p> <p>For implantable neural interface applications, it is important to compress data and analyze spike patterns across multiple channels in real time. Such a computational task for online neural data processing requires an innovative circuit-architecture level <span class="hlt">design</span> approach for low-power, <span class="hlt">robust</span> and area-efficient hardware implementation. Conventional microprocessor or Digital Signal Processing (DSP) chips would dissipate too much power and are too large in size for an implantable system. In this paper, we propose a novel hardware <span class="hlt">design</span> approach, referred to as "Preferential <span class="hlt">Design</span>" that exploits the nature of the neural signal processing algorithm to achieve a low-voltage, <span class="hlt">robust</span> and area-efficient implementation using nanoscale process technology. The basic idea is to isolate the critical components with respect to system performance and <span class="hlt">design</span> them more conservatively compared to the noncritical ones. This allows aggressive voltage scaling for low power operation while ensuring <span class="hlt">robustness</span> and area efficiency. We have applied the proposed approach to a neural signal processing algorithm using the Discrete Wavelet Transform (DWT) and observed significant improvement in power and <span class="hlt">robustness</span> over conventional <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20050082208&hterms=linear+programming&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dlinear%2Bprogramming','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20050082208&hterms=linear+programming&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dlinear%2Bprogramming"><span><span class="hlt">Robust</span> Control <span class="hlt">Design</span> via Linear Programming</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Keel, L. H.; Bhattacharyya, S. P.</p> <p>1998-01-01</p> <p>This paper deals with the problem of synthesizing or <span class="hlt">designing</span> a feedback controller of fixed dynamic order. The closed loop specifications considered here are given in terms of a target performance vector representing a desired set of closed loop transfer functions connecting various signals. In general these point targets are unattainable with a fixed order controller. By enlarging the target from a fixed point set to an interval set the solvability conditions with a fixed order controller are relaxed and a solution is more easily enabled. Results from the parametric <span class="hlt">robust</span> control literature can be used to <span class="hlt">design</span> the interval target family so that the performance deterioration is acceptable, even when plant uncertainty is present. It is shown that it is possible to devise a computationally simple linear programming approach that attempts to meet the desired closed loop specifications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27411334','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27411334"><span>Improved production of tannase by Klebsiella pneumoniae using Indian gooseberry leaves under submerged fermentation using <span class="hlt">Taguchi</span> approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kumar, Mukesh; Singh, Amrinder; Beniwal, Vikas; Salar, Raj Kumar</p> <p>2016-12-01</p> <p>Tannase (tannin acyl hydrolase E.C 3.1.1.20) is an inducible, largely extracellular enzyme that causes the hydrolysis of ester and depside bonds present in various substrates. Large scale industrial application of this enzyme is very limited owing to its high production costs. In the present study, cost effective production of tannase by Klebsiella pneumoniae KP715242 was studied under submerged fermentation using different tannin rich agro-residues like Indian gooseberry leaves (Phyllanthus emblica), Black plum leaves (Syzygium cumini), Eucalyptus leaves (Eucalyptus glogus) and Babul leaves (Acacia nilotica). Among all agro-residues, Indian gooseberry leaves were found to be the best substrate for tannase production under submerged fermentation. Sequential optimization approach using <span class="hlt">Taguchi</span> orthogonal array screening and response surface methodology was adopted to optimize the fermentation variables in order to enhance the enzyme production. Eleven medium components were screened primarily by <span class="hlt">Taguchi</span> orthogonal array <span class="hlt">design</span> to identify the most contributing factors towards the enzyme production. The four most significant contributing variables affecting tannase production were found to be pH (23.62 %), tannin extract (20.70 %), temperature (20.33 %) and incubation time (14.99 %). These factors were further optimized with central composite <span class="hlt">design</span> using response surface methodology. Maximum tannase production was observed at 5.52 pH, 39.72 °C temperature, 91.82 h of incubation time and 2.17 % tannin content. The enzyme activity was enhanced by 1.26 fold under these optimized conditions. The present study emphasizes the use of agro-residues as a potential substrate with an aim to lower down the input costs for tannase production so that the enzyme could be used proficiently for commercial purposes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22226460','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22226460"><span>Quality by <span class="hlt">Design</span>: Multidimensional exploration of the <span class="hlt">design</span> space in high performance liquid chromatography method development for better <span class="hlt">robustness</span> before validation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Monks, K; Molnár, I; Rieger, H-J; Bogáti, B; Szabó, E</p> <p>2012-04-06</p> <p><span class="hlt">Robust</span> HPLC separations lead to fewer analysis failures and better method transfer as well as providing an assurance of quality. This work presents the systematic development of an optimal, <span class="hlt">robust</span>, fast UHPLC method for the simultaneous assay of two APIs of an eye drop sample and their impurities, in accordance with Quality by <span class="hlt">Design</span> principles. Chromatography software is employed to effectively generate <span class="hlt">design</span> spaces (Method Operable <span class="hlt">Design</span> Regions), which are subsequently employed to determine the final method conditions and to evaluate <span class="hlt">robustness</span> prior to validation. Copyright © 2011 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..324a2054L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..324a2054L"><span>Optimisation Of Cutting Parameters Of Composite Material Laser Cutting Process By <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lokesh, S.; Niresh, J.; Neelakrishnan, S.; Rahul, S. P. Deepak</p> <p>2018-03-01</p> <p>The aim of this work is to develop a laser cutting process model that can predict the relationship between the process input parameters and resultant surface roughness, kerf width characteristics. The research conduct is based on the <span class="hlt">Design</span> of Experiment (DOE) analysis. Response Surface Methodology (RSM) is used in this work. It is one of the most practical and most effective techniques to develop a process model. Even though RSM has been used for the optimization of the laser process, this research investigates laser cutting of materials like Composite wood (veneer)to be best circumstances of laser cutting using RSM process. The input parameters evaluated are focal length, power supply and cutting speed, the output responses being kerf width, surface roughness, temperature. To efficiently optimize and customize the kerf width and surface roughness characteristics, a machine laser cutting process model using <span class="hlt">Taguchi</span> L9 orthogonal methodology was proposed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..314a2014M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..314a2014M"><span>Study of Dimple Effect on the Friction Characteristics of a Journal Bearing using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Murthy, A. Amar; Raghunandana, Dr.</p> <p>2018-02-01</p> <p>The effect of producing dimples using chemically etched techniques or by machining process on the surface of a journal bearing bushing to reduce the friction using <span class="hlt">Taguchi</span> method is investigated. The data used in the present analysis is based on the results obtained by the series of experiments conducted to study the dimples effect on the Stribeck curve. It is statistically proved that producing dimples on the bushing surface of a journal bearing has significant effect on the friction coefficient when used with light oils. Also it is seen that there is an interaction effect between speeds-load and load-dimples. Hence the interaction effect, which are usually neglected should be considered during actual experiments that significantly contributes in reducing the friction in mixed lubrication regime. The experiments, if were conducted after <span class="hlt">Taguchi</span> method, then the number of experiments would have been reduced to half of the actual set of experiments that were essentially conducted.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS.962a2010V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS.962a2010V"><span>Optimization of Parameters for Manufacture Nanopowder Bioceramics at Machine Pulverisette 6 by <span class="hlt">Taguchi</span> and ANOVA Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Van Hoten, Hendri; Gunawarman; Mulyadi, Ismet Hari; Kurniawan Mainil, Afdhal; Putra, Bismantoloa dan</p> <p>2018-02-01</p> <p>This research is about manufacture nanopowder Bioceramics from local materials used Ball Milling for biomedical applications. Source materials for the manufacture of medicines are plants, animal tissues, microbial structures and engineering biomaterial. The form of raw material medicines is a powder before mixed. In the case of medicines, research is to find sources of biomedical materials that will be in the nanoscale powders can be used as raw material for medicine. One of the biomedical materials that can be used as raw material for medicine is of the type of bioceramics is chicken eggshells. This research will develop methods for manufacture nanopowder material from chicken eggshells with Ball Milling using the <span class="hlt">Taguchi</span> method and ANOVA. Eggshell milled using a variation of Milling rate on 150, 200 and 250 rpm, the time variation of 1, 2 and 3 hours and variations the grinding balls to eggshell powder weight ratio (BPR) 1: 6, 1: 8, 1: 10. Before milled with Ball Milling crushed eggshells in advance and calcinate to a temperature of 900°C. After the milled material characterization of the fine powder of eggshell using SEM to see its size. The result of this research is optimum parameter of <span class="hlt">Taguchi</span> <span class="hlt">Design</span> analysis that is 250 rpm milling rate, 3 hours milling time and BPR is 1: 6 with the average eggshell powder size is 1.305 μm. Milling speed, milling time and ball to powder weight of ratio have contribution successively equal to 60.82%, 30.76% and 6.64% by error equal to 1.78%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/14528613','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/14528613"><span>[Development of an optimized formulation of damask marmalade with low energy level using <span class="hlt">Taguchi</span> methodology].</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Villarroel, Mario; Castro, Ruth; Junod, Julio</p> <p>2003-06-01</p> <p>The goal of this present study was the development of an optimized formula of damask marmalade low in calories applying <span class="hlt">Taguchi</span> methodology to improve the quality of this product. The selection of this methodology lies on the fact that in real life conditions the result of an experiment frequently depends on the influence of several variables, therefore, one expedite way to solve this problem is utilizing factorial desings. The influence of acid, thickener, sweetener and aroma additives, as well as time of cooking, and possible interactions among some of them, were studied trying to get the best combination of these factors to optimize the sensorial quality of an experimental formulation of dietetic damask marmalade. An orthogonal array L8 (2(7)) was applied in this experience, as well as level average analysis was carried out according <span class="hlt">Taguchi</span> methodology to determine the suitable working levels of the <span class="hlt">design</span> factors previously choiced, to achieve a desirable product quality. A sensory trained panel was utilized to analyze the marmalade samples using a composite scoring test with a descriptive acuantitative scale ranging from 1 = Bad, 5 = Good. It was demonstrated that the <span class="hlt">design</span> factors sugar/aspartame, pectin and damask aroma had a significant effect (p < 0.05) on the sensory quality of the marmalade with 82% of contribution on the response. The optimal combination result to be: citric acid 0.2%; pectin 1%; 30 g sugar/16 mg aspartame/100 g, damask aroma 0.5 ml/100 g, time of cooking 5 minutes. Regarding chemical composition, the most important results turned out to be the decrease in carbohydrate content compaired with traditional marmalade with a reduction of 56% in coloric value and also the amount of dietary fiber greater than similar commercial products. Assays of storage stability were carried out on marmalade samples submitted to different temperatures held in plastic bags of different density. Non percetible sensorial, microbiological and chemical changes</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_9 --> <div id="page_10" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="181"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26430454','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26430454"><span>Formulation and optimization of solid lipid nanoparticle formulation for pulmonary delivery of budesonide using <span class="hlt">Taguchi</span> and Box-Behnken <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Emami, J; Mohiti, H; Hamishehkar, H; Varshosaz, J</p> <p>2015-01-01</p> <p>Budesonide is a potent non-halogenated corticosteroid with high anti-inflammatory effects. The lungs are an attractive route for non-invasive drug delivery with advantages for both systemic and local applications. The aim of the present study was to develop, characterize and optimize a solid lipid nanoparticle system to deliver budesonide to the lungs. Budesonide-loaded solid lipid nanoparticles were prepared by the emulsification-solvent diffusion method. The impact of various processing variables including surfactant type and concentration, lipid content organic and aqueous volume, and sonication time were assessed on the particle size, zeta potential, entrapment efficiency, loading percent and mean dissolution time. <span class="hlt">Taguchi</span> <span class="hlt">design</span> with 12 formulations along with Box-Behnken <span class="hlt">design</span> with 17 formulations was developed. The impact of each factor upon the eventual responses was evaluated, and the optimized formulation was finally selected. The size and morphology of the prepared nanoparticles were studied using scanning electron microscope. Based on the optimization made by <span class="hlt">Design</span> Expert 7(®) software, a formulation made of glycerol monostearate, 1.2 % polyvinyl alcohol (PVA), weight ratio of lipid/drug of 10 and sonication time of 90 s was selected. Particle size, zeta potential, entrapment efficiency, loading percent, and mean dissolution time of adopted formulation were predicted and confirmed to be 218.2 ± 6.6 nm, -26.7 ± 1.9 mV, 92.5 ± 0.52 %, 5.8 ± 0.3 %, and 10.4 ± 0.29 h, respectively. Since the preparation and evaluation of the selected formulation within the laboratory yielded acceptable results with low error percent, the modeling and optimization was justified. The optimized formulation co-spray dried with lactose (hybrid microparticles) displayed desirable fine particle fraction, mass median aerodynamic diameter (MMAD), and geometric standard deviation of 49.5%, 2.06 μm, and 2.98 μm; respectively. Our results provide fundamental data for the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4578209','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4578209"><span>Formulation and optimization of solid lipid nanoparticle formulation for pulmonary delivery of budesonide using <span class="hlt">Taguchi</span> and Box-Behnken <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Emami, J.; Mohiti, H.; Hamishehkar, H.; Varshosaz, J.</p> <p>2015-01-01</p> <p>Budesonide is a potent non-halogenated corticosteroid with high anti-inflammatory effects. The lungs are an attractive route for non-invasive drug delivery with advantages for both systemic and local applications. The aim of the present study was to develop, characterize and optimize a solid lipid nanoparticle system to deliver budesonide to the lungs. Budesonide-loaded solid lipid nanoparticles were prepared by the emulsification-solvent diffusion method. The impact of various processing variables including surfactant type and concentration, lipid content organic and aqueous volume, and sonication time were assessed on the particle size, zeta potential, entrapment efficiency, loading percent and mean dissolution time. <span class="hlt">Taguchi</span> <span class="hlt">design</span> with 12 formulations along with Box-Behnken <span class="hlt">design</span> with 17 formulations was developed. The impact of each factor upon the eventual responses was evaluated, and the optimized formulation was finally selected. The size and morphology of the prepared nanoparticles were studied using scanning electron microscope. Based on the optimization made by <span class="hlt">Design</span> Expert 7® software, a formulation made of glycerol monostearate, 1.2 % polyvinyl alcohol (PVA), weight ratio of lipid/drug of 10 and sonication time of 90 s was selected. Particle size, zeta potential, entrapment efficiency, loading percent, and mean dissolution time of adopted formulation were predicted and confirmed to be 218.2 ± 6.6 nm, -26.7 ± 1.9 mV, 92.5 ± 0.52 %, 5.8 ± 0.3 %, and 10.4 ± 0.29 h, respectively. Since the preparation and evaluation of the selected formulation within the laboratory yielded acceptable results with low error percent, the modeling and optimization was justified. The optimized formulation co-spray dried with lactose (hybrid microparticles) displayed desirable fine particle fraction, mass median aerodynamic diameter (MMAD), and geometric standard deviation of 49.5%, 2.06 μm, and 2.98 μm; respectively. Our results provide fundamental data for the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009TJSAI..24...13S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009TJSAI..24...13S"><span>Real-World Application of <span class="hlt">Robust</span> <span class="hlt">Design</span> Optimization Assisted by Response Surface Approximation and Visual Data-Mining</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shimoyama, Koji; Jeong, Shinkyu; Obayashi, Shigeru</p> <p></p> <p>A new approach for multi-objective <span class="hlt">robust</span> <span class="hlt">design</span> optimization was proposed and applied to a real-world <span class="hlt">design</span> problem with a large number of objective functions. The present approach is assisted by response surface approximation and visual data-mining, and resulted in two major gains regarding computational time and data interpretation. The Kriging model for response surface approximation can markedly reduce the computational time for predictions of <span class="hlt">robustness</span>. In addition, the use of self-organizing maps as a data-mining technique allows visualization of complicated <span class="hlt">design</span> information between optimality and <span class="hlt">robustness</span> in a comprehensible two-dimensional form. Therefore, the extraction and interpretation of trade-off relations between optimality and <span class="hlt">robustness</span> of <span class="hlt">design</span>, and also the location of sweet spots in the <span class="hlt">design</span> space, can be performed in a comprehensive manner.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010JMSA....9...87C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010JMSA....9...87C"><span>H∞ <span class="hlt">robust</span> fault-tolerant controller <span class="hlt">design</span> for an autonomous underwater vehicle's navigation control system</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cheng, Xiang-Qin; Qu, Jing-Yuan; Yan, Zhe-Ping; Bian, Xin-Qian</p> <p>2010-03-01</p> <p>In order to improve the security and reliability for autonomous underwater vehicle (AUV) navigation, an H∞ <span class="hlt">robust</span> fault-tolerant controller was <span class="hlt">designed</span> after analyzing variations in state-feedback gain. Operating conditions and the <span class="hlt">design</span> method were then analyzed so that the control problem could be expressed as a mathematical optimization problem. This permitted the use of linear matrix inequalities (LMI) to solve for the H∞ controller for the system. When considering different actuator failures, these conditions were then also mathematically expressed, allowing the H∞ <span class="hlt">robust</span> controller to solve for these events and thus be fault-tolerant. Finally, simulation results showed that the H∞ <span class="hlt">robust</span> fault-tolerant controller could provide precise AUV navigation control with strong <span class="hlt">robustness</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJC....91..639R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJC....91..639R"><span><span class="hlt">Robust</span> synergetic control <span class="hlt">design</span> under inputs and states constraints</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rastegar, Saeid; Araújo, Rui; Sadati, Jalil</p> <p>2018-03-01</p> <p>In this paper, a novel <span class="hlt">robust</span>-constrained control methodology for discrete-time linear parameter-varying (DT-LPV) systems is proposed based on a synergetic control theory (SCT) approach. It is shown that in DT-LPV systems without uncertainty, and for any unmeasured bounded additive disturbance, the proposed controller accomplishes the goal of stabilising the system by asymptotically driving the error of the controlled variable to a bounded set containing the origin and then maintaining it there. Moreover, given an uncertain DT-LPV system jointly subject to unmeasured and constrained additive disturbances, and constraints in states, input commands and reference signals (set points), then invariant set theory is used to find an appropriate polyhedral <span class="hlt">robust</span> invariant region in which the proposed control framework is guaranteed to <span class="hlt">robustly</span> stabilise the closed-loop system. Furthermore, this is achieved even for the case of varying non-zero control set points in such uncertain DT-LPV systems. The controller is characterised to have a simple structure leading to an easy implementation, and a non-complex <span class="hlt">design</span> process. The effectiveness of the proposed method and the implications of the controller <span class="hlt">design</span> on feasibility and closed-loop performance are demonstrated through application examples on the temperature control on a continuous-stirred tank reactor plant, on the control of a real-coupled DC motor plant, and on an open-loop unstable system example.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012EPJB...85..129K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012EPJB...85..129K"><span><span class="hlt">Design</span> of <span class="hlt">robust</span> flow processing networks with time-programmed responses</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kaluza, P.; Mikhailov, A. S.</p> <p>2012-04-01</p> <p>Can artificially <span class="hlt">designed</span> networks reach the levels of <span class="hlt">robustness</span> against local damage which are comparable with those of the biochemical networks of a living cell? We consider a simple model where the flow applied to an input node propagates through the network and arrives at different times to the output nodes, thus generating a pattern of coordinated responses. By using evolutionary optimization algorithms, functional networks - with required time-programmed responses - were constructed. Then, continuing the evolution, such networks were additionally optimized for <span class="hlt">robustness</span> against deletion of individual nodes or links. In this manner, large ensembles of functional networks with different kinds of <span class="hlt">robustness</span> were obtained, making statistical investigations and comparison of their structural properties possible. We have found that, generally, different architectures are needed for various kinds of <span class="hlt">robustness</span>. The differences are statistically revealed, for example, in the Laplacian spectra of the respective graphs. On the other hand, motif distributions of <span class="hlt">robust</span> networks do not differ from those of the merely functional networks; they are found to belong to the first Alon superfamily, the same as that of the gene transcription networks of single-cell organisms.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJSS...49..211H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJSS...49..211H"><span>A <span class="hlt">robust</span> fractional-order PID controller <span class="hlt">design</span> based on active queue management for TCP network</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hamidian, Hamideh; Beheshti, Mohammad T. H.</p> <p>2018-01-01</p> <p>In this paper, a <span class="hlt">robust</span> fractional-order controller is <span class="hlt">designed</span> to control the congestion in transmission control protocol (TCP) networks with time-varying parameters. Fractional controllers can increase the stability and <span class="hlt">robustness</span>. Regardless of advantages of fractional controllers, they are still not common in congestion control in TCP networks. The network parameters are time-varying, so the <span class="hlt">robust</span> stability is important in congestion controller <span class="hlt">design</span>. Therefore, we focused on the <span class="hlt">robust</span> controller <span class="hlt">design</span>. The fractional PID controller is developed based on active queue management (AQM). D-partition technique is used. The most important property of <span class="hlt">designed</span> controller is the <span class="hlt">robustness</span> to the time-varying parameters of the TCP network. The vertex quasi-polynomials of the closed-loop characteristic equation are obtained, and the stability boundaries are calculated for each vertex quasi-polynomial. The intersection of all stability regions is insensitive to network parameter variations, and results in <span class="hlt">robust</span> stability of TCP/AQM system. NS-2 simulations show that the proposed algorithm provides a stable queue length. Moreover, simulations show smaller oscillations of the queue length and less packet drop probability for FPID compared to PI and PID controllers. We can conclude from NS-2 simulations that the average packet loss probability variations are negligible when the network parameters change.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ResPh...7.3287G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ResPh...7.3287G"><span>Absolute variation of the mechanical characteristics of halloysite reinforced polyurethane nanocomposites complemented by <span class="hlt">Taguchi</span> and ANOVA approaches</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gaaz, Tayser Sumer; Sulong, Abu Bakar; Kadhum, Abdul Amir H.; Nassir, Mohamed H.; Al-Amiery, Ahmed A.</p> <p></p> <p>The variation of the results of the mechanical properties of halloysite nanotubes (HNTs) reinforced thermoplastic polyurethane (TPU) at different HNTs loadings was implemented as a tool for analysis. The preparation of HNTs-TPU nanocomposites was performed under four controlled parameters of mixing temperature, mixing speed, mixing time, and HNTs loading at three levels each to satisfy <span class="hlt">Taguchi</span> method orthogonal array L9 aiming to optimize these parameters for the best measurements of tensile strength, Young's modulus, and tensile strain (known as responses). The maximum variation of the experimental results for each response was determined and analysed based on the optimized results predicted by <span class="hlt">Taguchi</span> method and ANOVA. It was found that the maximum absolute variations of the three mentioned responses are 69%, 352%, and 126%, respectively. The analysis has shown that the preparation of the optimized tensile strength requires 1 wt.% HNTs loading (excluding 2 wt.% and 3 wt.%), mixing temperature of 190 °C (excluding 200 °C and 210 °C), and mixing speed of 30 rpm (excluding 40 rpm and 50 rpm). In addition, the analysis has determined that the mixing time at 20 min has no effect on the preparation. The mentioned analysis was fortified by ANOVA, images of FESEM, and DSC results. Seemingly, the agglomeration and distribution of HNTs in the nanocomposite play an important role in the process. The outcome of the analysis could be considered as a very important step towards the reliability of <span class="hlt">Taguchi</span> method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24683334','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24683334"><span>Multiobjective <span class="hlt">robust</span> <span class="hlt">design</span> of the double wishbone suspension system based on particle swarm optimization.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Cheng, Xianfu; Lin, Yuqun</p> <p>2014-01-01</p> <p>The performance of the suspension system is one of the most important factors in the vehicle <span class="hlt">design</span>. For the double wishbone suspension system, the conventional deterministic optimization does not consider any deviations of <span class="hlt">design</span> parameters, so <span class="hlt">design</span> sensitivity analysis and <span class="hlt">robust</span> optimization <span class="hlt">design</span> are proposed. In this study, the <span class="hlt">design</span> parameters of the <span class="hlt">robust</span> optimization are the positions of the key points, and the random factors are the uncertainties in manufacturing. A simplified model of the double wishbone suspension is established by software ADAMS. The sensitivity analysis is utilized to determine main <span class="hlt">design</span> variables. Then, the simulation experiment is arranged and the Latin hypercube <span class="hlt">design</span> is adopted to find the initial points. The Kriging model is employed for fitting the mean and variance of the quality characteristics according to the simulation results. Further, a particle swarm optimization method based on simple PSO is applied and the tradeoff between the mean and deviation of performance is made to solve the <span class="hlt">robust</span> optimization problem of the double wishbone suspension system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930017894','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930017894"><span><span class="hlt">Robust</span> controller <span class="hlt">design</span> for flexible structures using normalized coprime factor plant descriptions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Armstrong, Ernest S.</p> <p>1993-01-01</p> <p>Stabilization is a fundamental requirement in the <span class="hlt">design</span> of feedback compensators for flexible structures. The search for the largest neighborhood around a given <span class="hlt">design</span> plant for which a single controller produces closed-loop stability can be formulated as an H(sub infinity) control problem. The use of normalized coprime factor plant descriptions, in which the plant perturbations are defined as additive modifications to the coprime factors, leads to a closed-form expression for the maximum neighborhood boundary allowing optimal and suboptimal H(sub infinity) compensators to be computed directly without the usual gamma iteration. A summary of the theory on <span class="hlt">robust</span> stabilization using normalized coprime factor plant descriptions is presented, and the application of the theory to the computation of <span class="hlt">robustly</span> stable compensators for the phase version of the Control-Structures Interaction (CSI) Evolutionary Model is described. Results from the application indicate that the suboptimal version of the theory has the potential of providing the bases for the computation of low-authority compensators that are <span class="hlt">robustly</span> stable to expected variations in <span class="hlt">design</span> model parameters and additive unmodeled dynamics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860021793','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860021793"><span>Control <span class="hlt">design</span> for <span class="hlt">robust</span> stability in linear regulators: Application to aerospace flight control</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yedavalli, R. K.</p> <p>1986-01-01</p> <p>Time domain stability <span class="hlt">robustness</span> analysis and <span class="hlt">design</span> for linear multivariable uncertain systems with bounded uncertainties is the central theme of the research. After reviewing the recently developed upper bounds on the linear elemental (structured), time varying perturbation of an asymptotically stable linear time invariant regulator, it is shown that it is possible to further improve these bounds by employing state transformations. Then introducing a quantitative measure called the stability <span class="hlt">robustness</span> index, a state feedback conrol <span class="hlt">design</span> algorithm is presented for a general linear regulator problem and then specialized to the case of modal systems as well as matched systems. The extension of the algorithm to stochastic systems with Kalman filter as the state estimator is presented. Finally an algorithm for <span class="hlt">robust</span> dynamic compensator <span class="hlt">design</span> is presented using Parameter Optimization (PO) procedure. Applications in a aircraft control and flexible structure control are presented along with a comparison with other existing methods.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1902b0034S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1902b0034S"><span>The <span class="hlt">robust</span> corrective action priority-an improved approach for selecting competing corrective actions in FMEA based on principle of <span class="hlt">robust</span> <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sutrisno, Agung; Gunawan, Indra; Vanany, Iwan</p> <p>2017-11-01</p> <p>In spite of being integral part in risk - based quality improvement effort, studies improving quality of selection of corrective action priority using FMEA technique are still limited in literature. If any, none is considering <span class="hlt">robustness</span> and risk in selecting competing improvement initiatives. This study proposed a theoretical model to select risk - based competing corrective action by considering <span class="hlt">robustness</span> and risk of competing corrective actions. We incorporated the principle of <span class="hlt">robust</span> <span class="hlt">design</span> in counting the preference score among corrective action candidates. Along with considering cost and benefit of competing corrective actions, we also incorporate the risk and <span class="hlt">robustness</span> of corrective actions. An example is provided to represent the applicability of the proposed model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19940004705&hterms=entropy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dentropy','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19940004705&hterms=entropy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dentropy"><span>A homotopy algorithm for synthesizing <span class="hlt">robust</span> controllers for flexible structures via the maximum entropy <span class="hlt">design</span> equations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Collins, Emmanuel G., Jr.; Richter, Stephen</p> <p>1990-01-01</p> <p>One well known deficiency of LQG compensators is that they do not guarantee any measure of <span class="hlt">robustness</span>. This deficiency is especially highlighted when considering control <span class="hlt">design</span> for complex systems such as flexible structures. There has thus been a need to generalize LQG theory to incorporate <span class="hlt">robustness</span> constraints. Here we describe the maximum entropy approach to <span class="hlt">robust</span> control <span class="hlt">design</span> for flexible structures, a generalization of LQG theory, pioneered by Hyland, which has proved useful in practice. The <span class="hlt">design</span> equations consist of a set of coupled Riccati and Lyapunov equations. A homotopy algorithm that is used to solve these <span class="hlt">design</span> equations is presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030068105','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030068105"><span>The Role of <span class="hlt">Design</span>-of-Experiments in Managing Flow in Compact Air Vehicle Inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anderson, Bernhard H.; Miller, Daniel N.; Gridley, Marvin C.; Agrell, Johan</p> <p>2003-01-01</p> <p>It is the purpose of this study to demonstrate the viability and economy of <span class="hlt">Design</span>-of-Experiments methodologies to arrive at microscale secondary flow control array <span class="hlt">designs</span> that maintain optimal inlet performance over a wide range of the mission variables and to explore how these statistical methods provide a better understanding of the management of flow in compact air vehicle inlets. These statistical <span class="hlt">design</span> concepts were used to investigate the <span class="hlt">robustness</span> properties of low unit strength micro-effector arrays. Low unit strength micro-effectors are micro-vanes set at very low angles-of-incidence with very long chord lengths. They were <span class="hlt">designed</span> to influence the near wall inlet flow over an extended streamwise distance, and their advantage lies in low total pressure loss and high effectiveness in managing engine face distortion. The term <span class="hlt">robustness</span> is used in this paper in the same sense as it is used in the industrial problem solving community. It refers to minimizing the effects of the hard-to-control factors that influence the development of a product or process. In <span class="hlt">Robustness</span> Engineering, the effects of the hard-to-control factors are often called noise , and the hard-to-control factors themselves are referred to as the environmental variables or sometimes as the <span class="hlt">Taguchi</span> noise variables. Hence <span class="hlt">Robust</span> Optimization refers to minimizing the effects of the environmental or noise variables on the development (<span class="hlt">design</span>) of a product or process. In the management of flow in compact inlets, the environmental or noise variables can be identified with the mission variables. Therefore this paper formulates a statistical <span class="hlt">design</span> methodology that minimizes the impact of variations in the mission variables on inlet performance and demonstrates that these statistical <span class="hlt">design</span> concepts can lead to simpler inlet flow management systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20160008094','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20160008094"><span><span class="hlt">Designing</span> for Reliability and <span class="hlt">Robustness</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Svetlik, Randall G.; Moore, Cherice; Williams, Antony</p> <p>2017-01-01</p> <p>Long duration spaceflight has a negative effect on the human body, and exercise countermeasures are used on-board the International Space Station (ISS) to minimize bone and muscle loss, combatting these effects. Given the importance of these hardware systems to the health of the crew, this equipment must continue to be readily available. <span class="hlt">Designing</span> spaceflight exercise hardware to meet high reliability and availability standards has proven to be challenging throughout the time the crewmembers have been living on ISS beginning in 2000. Furthermore, restoring operational capability after a failure is clearly time-critical, but can be problematic given the challenges of troubleshooting the problem from 220 miles away. Several best-practices have been leveraged in seeking to maximize availability of these exercise systems, including <span class="hlt">designing</span> for <span class="hlt">robustness</span>, implementing diagnostic instrumentation, relying on user feedback, and providing ample maintenance and sparing. These factors have enhanced the reliability of hardware systems, and therefore have contributed to keeping the crewmembers healthy upon return to Earth. This paper will review the failure history for three spaceflight exercise countermeasure systems identifying lessons learned that can help improve future systems. Specifically, the Treadmill with Vibration Isolation and Stabilization System (TVIS), Cycle Ergometer with Vibration Isolation and Stabilization System (CEVIS), and the Advanced Resistive Exercise Device (ARED) will be reviewed, analyzed, and conclusions identified so as to provide guidance for improving future exercise hardware <span class="hlt">designs</span>. These lessons learned, paired with thorough testing, offer a path towards reduced system down-time.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..269a2066Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..269a2066Z"><span><span class="hlt">Robust</span> Optimization <span class="hlt">Design</span> for Turbine Blade-Tip Radial Running Clearance using Hierarchically Response Surface Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhiying, Chen; Ping, Zhou</p> <p>2017-11-01</p> <p>Considering the <span class="hlt">robust</span> optimization computational precision and efficiency for complex mechanical assembly relationship like turbine blade-tip radial running clearance, a hierarchically response surface <span class="hlt">robust</span> optimization algorithm is proposed. The distribute collaborative response surface method is used to generate assembly system level approximation model of overall parameters and blade-tip clearance, and then a set samples of <span class="hlt">design</span> parameters and objective response mean and/or standard deviation is generated by using system approximation model and <span class="hlt">design</span> of experiment method. Finally, a new response surface approximation model is constructed by using those samples, and this approximation model is used for <span class="hlt">robust</span> optimization process. The analyses results demonstrate the proposed method can dramatic reduce the computational cost and ensure the computational precision. The presented research offers an effective way for the <span class="hlt">robust</span> optimization <span class="hlt">design</span> of turbine blade-tip radial running clearance.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23047554','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23047554"><span>Optimal <span class="hlt">design</span> of stimulus experiments for <span class="hlt">robust</span> discrimination of biochemical reaction networks.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Flassig, R J; Sundmacher, K</p> <p>2012-12-01</p> <p>Biochemical reaction networks in the form of coupled ordinary differential equations (ODEs) provide a powerful modeling tool for understanding the dynamics of biochemical processes. During the early phase of modeling, scientists have to deal with a large pool of competing nonlinear models. At this point, discrimination experiments can be <span class="hlt">designed</span> and conducted to obtain optimal data for selecting the most plausible model. Since biological ODE models have widely distributed parameters due to, e.g. biologic variability or experimental variations, model responses become distributed. Therefore, a <span class="hlt">robust</span> optimal experimental <span class="hlt">design</span> (OED) for model discrimination can be used to discriminate models based on their response probability distribution functions (PDFs). In this work, we present an optimal control-based methodology for <span class="hlt">designing</span> optimal stimulus experiments aimed at <span class="hlt">robust</span> model discrimination. For estimating the time-varying model response PDF, which results from the nonlinear propagation of the parameter PDF under the ODE dynamics, we suggest using the sigma-point approach. Using the model overlap (expected likelihood) as a <span class="hlt">robust</span> discrimination criterion to measure dissimilarities between expected model response PDFs, we benchmark the proposed nonlinear <span class="hlt">design</span> approach against linearization with respect to prediction accuracy and <span class="hlt">design</span> quality for two nonlinear biological reaction networks. As shown, the sigma-point outperforms the linearization approach in the case of widely distributed parameter sets and/or existing multiple steady states. Since the sigma-point approach scales linearly with the number of model parameter, it can be applied to large systems for <span class="hlt">robust</span> experimental planning. An implementation of the method in MATLAB/AMPL is available at http://www.uni-magdeburg.de/ivt/svt/person/rf/roed.html. flassig@mpi-magdeburg.mpg.de Supplementary data are are available at Bioinformatics online.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhDT.......147G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhDT.......147G"><span>A <span class="hlt">Robust</span> Adaptive Autonomous Approach to Optimal Experimental <span class="hlt">Design</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gu, Hairong</p> <p></p> <p>Experimentation is the fundamental tool of scientific inquiries to understand the laws governing the nature and human behaviors. Many complex real-world experimental scenarios, particularly in quest of prediction accuracy, often encounter difficulties to conduct experiments using an existing experimental procedure for the following two reasons. First, the existing experimental procedures require a parametric model to serve as the proxy of the latent data structure or data-generating mechanism at the beginning of an experiment. However, for those experimental scenarios of concern, a sound model is often unavailable before an experiment. Second, those experimental scenarios usually contain a large number of <span class="hlt">design</span> variables, which potentially leads to a lengthy and costly data collection cycle. Incompetently, the existing experimental procedures are unable to optimize large-scale experiments so as to minimize the experimental length and cost. Facing the two challenges in those experimental scenarios, the aim of the present study is to develop a new experimental procedure that allows an experiment to be conducted without the assumption of a parametric model while still achieving satisfactory prediction, and performs optimization of experimental <span class="hlt">designs</span> to improve the efficiency of an experiment. The new experimental procedure developed in the present study is named <span class="hlt">robust</span> adaptive autonomous system (RAAS). RAAS is a procedure for sequential experiments composed of multiple experimental trials, which performs function estimation, variable selection, reverse prediction and <span class="hlt">design</span> optimization on each trial. Directly addressing the challenges in those experimental scenarios of concern, function estimation and variable selection are performed by data-driven modeling methods to generate a predictive model from data collected during the course of an experiment, thus exempting the requirement of a parametric model at the beginning of an experiment; <span class="hlt">design</span> optimization is</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940020626','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940020626"><span><span class="hlt">Robust</span>, nonlinear, high angle-of-attack control <span class="hlt">design</span> for a supermaneuverable vehicle</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Adams, Richard J.</p> <p>1993-01-01</p> <p>High angle-of-attack flight control laws are developed for a supermaneuverable fighter aircraft. The methods of dynamic inversion and structured singular value synthesis are combined into an approach which addresses both the nonlinearity and <span class="hlt">robustness</span> problems of flight at extreme operating conditions. The primary purpose of the dynamic inversion control elements is to linearize the vehicle response across the flight envelope. Structured singular value synthesis is used to <span class="hlt">design</span> a dynamic controller which provides <span class="hlt">robust</span> tracking to pilot commands. The resulting control system achieves desired flying qualities and guarantees a large margin of <span class="hlt">robustness</span> to uncertainties for high angle-of-attack flight conditions. The results of linear simulation and structured singular value stability analysis are presented to demonstrate satisfaction of the <span class="hlt">design</span> criteria. High fidelity nonlinear simulation results show that the combined dynamics inversion/structured singular value synthesis control law achieves a high level of performance in a realistic environment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29447441','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29447441"><span><span class="hlt">Design</span> factors of femur fracture fixation plates made of shape memory alloy based on the <span class="hlt">Taguchi</span> method by finite element analysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ko, Cheolwoong; Yang, Mikyung; Byun, Taemin; Lee, Sang-Wook</p> <p>2018-05-01</p> <p>This study proposed a way to <span class="hlt">design</span> femur fracture fixation plates made of shape memory alloy based on computed tomography (CT) images of Korean cadaveric femurs. To this end, 3 major <span class="hlt">design</span> factors of femur fracture fixation plates (circumference angle, thickness, and inner diameter) were selected based on the contact pressure when a femur fracture fixation plate was applied to a cylinder model using the <span class="hlt">Taguchi</span> method. Then, the effects of the <span class="hlt">design</span> factors were analyzed. It was shown that the <span class="hlt">design</span> factors were statistically significant at a level of p = 0.05 concerning the inner diameter and the thickness. The factors affecting the contact pressure were inner diameter, thickness, and circumference angle, in that order. Particularly, in the condition of Case 9 (inner diameter 27 mm, thickness 2.4 mm, and circumference angle 270°), the max. average contact pressure was 21.721 MPa, while the min. average contact pressure was 3.118 MPa in Case 10 (inner diameter 29 mm, thickness 2.0 mm, and circumference angle 210°). When the femur fracture fixation plate was applied to the cylinder model, the displacement due to external sliding and pulling forces was analyzed. As a result, the displacement in the sliding condition was at max. 3.75 times greater than that in the pulling condition, which indicated that the cohesion strength between the femur fracture fixation plate and the cylinder model was likely to be greater in the pulling condition. When a human femur model was applied, the max. average contact pressure was 10.76 MPa, which was lower than the yield strength of a human femur (108 MPa). In addition, the analysis of the rib behaviors of the femur fracture fixation plate in relation to the recovery effect of the shape memory alloy showed that the rib behaviors varied depending on the arbitrarily curved shapes of the femur sections. Copyright © 2018 John Wiley & Sons, Ltd.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_10 --> <div id="page_11" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="201"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..209a2081T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..209a2081T"><span>Using Quality Management Methods in Knowledge-Based Organizations. An Approach to the Application of the <span class="hlt">Taguchi</span> Method to the Process of Pressing Tappets into Anchors</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ţîţu, M. A.; Pop, A. B.; Ţîţu, Ș</p> <p>2017-06-01</p> <p>This paper presents a study on the modelling and optimization of certain variables by using the <span class="hlt">Taguchi</span> Method with a view to modelling and optimizing the process of pressing tappets into anchors, process conducted in an organization that promotes knowledge-based management. The paper promotes practical concepts of the <span class="hlt">Taguchi</span> Method and describes the way in which the objective functions are obtained and used during the modelling and optimization of the process of pressing tappets into the anchors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016MS%26E..149a2004M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016MS%26E..149a2004M"><span>Wear behavior of electroless Ni-P-W coating under lubricated condition - a <span class="hlt">Taguchi</span> based approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mukhopadhyay, Arkadeb; Duari, Santanu; Barman, Tapan Kumar; Sahoo, Prasanta</p> <p>2016-09-01</p> <p>The present study aims to investigate the tribological behavior of electroless Ni-P-W coating under engine oil lubricated condition to ascertain its suitability in automotive applications. Coating is deposited onto mild steel specimens by the electroless method. The experiments are carried out on a pin - on - disc type tribo tester under lubrication. Three tribotesting parameters namely the applied normal load, sliding speed and sliding duration are varied at their three levels and their effects on the wear depth of the deposits are studied. The experiments are carried out based on the combinations available in <span class="hlt">Taguchi</span>'s L27 orthogonal array (OA). Optimization of the tribo-testing parameters is carried out using <span class="hlt">Taguchi</span>'s S/N ratio method to minimize the wear depth. Analysis of variance carried out at a confidence level of 99% indicates that the sliding speed is the most significant parameter in controlling the wear behavior of the deposits. Coating characterization is done using scanning electron microscope, energy dispersive X-ray analysis and X-ray diffraction techniques. It is seen that the wear mechanism under lubricated condition is abrasive in nature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016SPJCE..11..119N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016SPJCE..11..119N"><span>Experimental study of optimal self compacting concrete with spent foundry sand as partial replacement for M-sand using <span class="hlt">Taguchi</span> approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nirmala, D. B.; Raviraj, S.</p> <p>2016-06-01</p> <p>This paper presents the application of <span class="hlt">Taguchi</span> approach to obtain optimal mix proportion for Self Compacting Concrete (SCC) containing spent foundry sand and M-sand. Spent foundry sand is used as a partial replacement for M-sand. The SCC mix has seven control factors namely, Coarse aggregate, M-sand with Spent Foundry sand, Cement, Fly ash, Water, Super plasticizer and Viscosity modifying agent. Modified Nan Su method is used to proportion the initial SCC mix. L18 (21×37) Orthogonal Arrays (OA) with the seven control factors having 3 levels is used in <span class="hlt">Taguchi</span> approach which resulted in 18 SCC mix proportions. All mixtures are extensively tested both in fresh and hardened states to verify whether they meet the practical and technical requirements of SCC. The quality characteristics considering "Nominal the better" situation is applied to the test results to arrive at the optimal SCC mix proportion. Test results indicate that the optimal mix satisfies the requirements of fresh and hardened properties of SCC. The study reveals the feasibility of using spent foundry sand as a partial replacement of M-sand in SCC and also that <span class="hlt">Taguchi</span> method is a reliable tool to arrive at optimal mix proportion of SCC.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20110013156&hterms=exogenous&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Dexogenous','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20110013156&hterms=exogenous&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Dexogenous"><span><span class="hlt">Robust</span> Path Planning and Feedback <span class="hlt">Design</span> Under Stochastic Uncertainty</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Blackmore, Lars</p> <p>2008-01-01</p> <p>Autonomous vehicles require optimal path planning algorithms to achieve mission goals while avoiding obstacles and being <span class="hlt">robust</span> to uncertainties. The uncertainties arise from exogenous disturbances, modeling errors, and sensor noise, which can be characterized via stochastic models. Previous work defined a notion of <span class="hlt">robustness</span> in a stochastic setting by using the concept of chance constraints. This requires that mission constraint violation can occur with a probability less than a prescribed value.In this paper we describe a novel method for optimal chance constrained path planning with feedback <span class="hlt">design</span>. The approach optimizes both the reference trajectory to be followed and the feedback controller used to reject uncertainty. Our method extends recent results in constrained control synthesis based on convex optimization to solve control problems with nonconvex constraints. This extension is essential for path planning problems, which inherently have nonconvex obstacle avoidance constraints. Unlike previous approaches to chance constrained path planning, the new approach optimizes the feedback gain as wellas the reference trajectory.The key idea is to couple a fast, nonconvex solver that does not take into account uncertainty, with existing <span class="hlt">robust</span> approaches that apply only to convex feasible regions. By alternating between <span class="hlt">robust</span> and nonrobust solutions, the new algorithm guarantees convergence to a global optimum. We apply the new method to an unmanned aircraft and show simulation results that demonstrate the efficacy of the approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19830060459&hterms=value+use&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dvalue%2Buse','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19830060459&hterms=value+use&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dvalue%2Buse"><span>The use of singular value gradients and optimization techniques to <span class="hlt">design</span> <span class="hlt">robust</span> controllers for multiloop systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Newsom, J. R.; Mukhopadhyay, V.</p> <p>1983-01-01</p> <p>A method for <span class="hlt">designing</span> <span class="hlt">robust</span> feedback controllers for multiloop systems is presented. <span class="hlt">Robustness</span> is characterized in terms of the minimum singular value of the system return difference matrix at the plant input. Analytical gradients of the singular values with respect to <span class="hlt">design</span> variables in the controller are derived. A cumulative measure of the singular values and their gradients with respect to the <span class="hlt">design</span> variables is used with a numerical optimization technique to increase the system's <span class="hlt">robustness</span>. Both unconstrained and constrained optimization techniques are evaluated. Numerical results are presented for a two-input/two-output drone flight control system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19840003747','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19840003747"><span>The use of singular value gradients and optimization techniques to <span class="hlt">design</span> <span class="hlt">robust</span> controllers for multiloop systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Newsom, J. R.; Mukhopadhyay, V.</p> <p>1983-01-01</p> <p>A method for <span class="hlt">designing</span> <span class="hlt">robust</span> feedback controllers for multiloop systems is presented. <span class="hlt">Robustness</span> is characterized in terms of the minimum singular value of the system return difference matrix at the plant input. Analytical gradients of the singular values with respect to <span class="hlt">design</span> variables in the controller are derived. A cumulative measure of the singular values and their gradients with respect to the <span class="hlt">design</span> variables is used with a numerical optimization technique to increase the system's <span class="hlt">robustness</span>. Both unconstrained and constrained optimization techniques are evaluated. Numerical results are presented for a two output drone flight control system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29691029','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29691029"><span>Preparation of nanocellulose from Imperata brasiliensis grass using <span class="hlt">Taguchi</span> method.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Benini, Kelly Cristina Coelho de Carvalho; Voorwald, Herman Jacobus Cornelis; Cioffi, Maria Odila Hilário; Rezende, Mirabel Cerqueira; Arantes, Valdeir</p> <p>2018-07-15</p> <p>Cellulose nanoparticles (CNs) were prepared by acid hydrolysis of the cellulose pulp extracted from the Brazilian satintail (Imperata Brasiliensis) plant using a conventional and a total chlorine free method. Initially, a statistical <span class="hlt">design</span> of experiment was carried out using <span class="hlt">Taguchi</span> orthogonal array to study the hydrolysis parameters, and the main properties (crystallinity, thermal stability, morphology, and sizes) of the nanocellulose. X-ray diffraction (XRD), fourier-transform infrared spectroscopy (FTIR), field-emission scanning electron microscopy (FE-SEM), dynamic light scattering (DLS), zeta potential and thermogravimetric analysis (TGA) were carried out to characterize the physical-chemical properties of the CNs obtained. Cellulose nanoparticles with diameter ranging from 10 to 60 nm and length between 150 and 250 nm were successfully obtained at sulfuric acid concentration of 64% (m/m), temperature 35 °C, reaction time 75 min, and a 1:20 (g/mL) pulp-to-solution ratio. Under this condition, the Imperata Brasiliensis CNs showed good stability in suspension, crystallinity index of 65%, and a cellulose degradation temperature of about 117 °C. Considering that these properties are similar to those of nanocelluloses from other lignocellulosics feedstocks, Imperata grass seems also to be a suitable source for nanocellulose production. Copyright © 2018 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19990087082&hterms=business+expenses&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbusiness%2Bexpenses','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19990087082&hterms=business+expenses&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dbusiness%2Bexpenses"><span>Hierarchical Modeling and <span class="hlt">Robust</span> Synthesis for the Preliminary <span class="hlt">Design</span> of Large Scale Complex Systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Koch, Patrick N.</p> <p>1997-01-01</p> <p>Large-scale complex systems are characterized by multiple interacting subsystems and the analysis of multiple disciplines. The <span class="hlt">design</span> and development of such systems inevitably requires the resolution of multiple conflicting objectives. The size of complex systems, however, prohibits the development of comprehensive system models, and thus these systems must be partitioned into their constituent parts. Because simultaneous solution of individual subsystem models is often not manageable iteration is inevitable and often excessive. In this dissertation these issues are addressed through the development of a method for hierarchical <span class="hlt">robust</span> preliminary <span class="hlt">design</span> exploration to facilitate concurrent system and subsystem <span class="hlt">design</span> exploration, for the concurrent generation of <span class="hlt">robust</span> system and subsystem specifications for the preliminary <span class="hlt">design</span> of multi-level, multi-objective, large-scale complex systems. This method is developed through the integration and expansion of current <span class="hlt">design</span> techniques: Hierarchical partitioning and modeling techniques for partitioning large-scale complex systems into more tractable parts, and allowing integration of subproblems for system synthesis; Statistical experimentation and approximation techniques for increasing both the efficiency and the comprehensiveness of preliminary <span class="hlt">design</span> exploration; and Noise modeling techniques for implementing <span class="hlt">robust</span> preliminary <span class="hlt">design</span> when approximate models are employed. Hierarchical partitioning and modeling techniques including intermediate responses, linking variables, and compatibility constraints are incorporated within a hierarchical compromise decision support problem formulation for synthesizing subproblem solutions for a partitioned system. Experimentation and approximation techniques are employed for concurrent investigations and modeling of partitioned subproblems. A modified composite experiment is introduced for fitting better predictive models across the ranges of the factors, and an approach for</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/5210630','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/5210630"><span>The '<span class="hlt">robust</span>' capture-recapture <span class="hlt">design</span> allows components of recruitment to be estimated</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Pollock, K.H.; Kendall, W.L.; Nichols, J.D.; Lebreton, J.-D.; North, P.M.</p> <p>1993-01-01</p> <p>The '<span class="hlt">robust</span>' capture-recapture <span class="hlt">design</span> (Pollock 1982) allows analyses which combine features of closed population model analyses (Otis et aI., 1978, White et aI., 1982) and open population model analyses (Pollock et aI., 1990). Estimators obtained under these analyses are more <span class="hlt">robust</span> to unequal catch ability than traditional Jolly-Seber estimators (Pollock, 1982; Pollock et al., 1990; Kendall, 1992). The <span class="hlt">robust</span> <span class="hlt">design</span> also allows estimation of parameters for population size, survival rate and recruitment numbers for all periods of the study unlike under Jolly-Seber type models. The major advantage of this <span class="hlt">design</span> that we emphasize in this short review paper is that it allows separate estimation of immigration and in situ recruitment numbers for a two or more age class model (Nichols and Pollock, 1990). This is contrasted with the age-dependent Jolly-Seber model (Pollock, 1981; Stokes, 1984; Pollock et L, 1990) which provides separate estimates for immigration and in situ recruitment for all but the first two age classes where there is at least a three age class model. The ability to achieve this separation of recruitment components can be very important to population modelers and wildlife managers as many species can only be separated into two easily identified age classes in the field.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1998PhDT.......196K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1998PhDT.......196K"><span>Hierarchical modeling and <span class="hlt">robust</span> synthesis for the preliminary <span class="hlt">design</span> of large scale complex systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Koch, Patrick Nathan</p> <p></p> <p>Large-scale complex systems are characterized by multiple interacting subsystems and the analysis of multiple disciplines. The <span class="hlt">design</span> and development of such systems inevitably requires the resolution of multiple conflicting objectives. The size of complex systems, however, prohibits the development of comprehensive system models, and thus these systems must be partitioned into their constituent parts. Because simultaneous solution of individual subsystem models is often not manageable iteration is inevitable and often excessive. In this dissertation these issues are addressed through the development of a method for hierarchical <span class="hlt">robust</span> preliminary <span class="hlt">design</span> exploration to facilitate concurrent system and subsystem <span class="hlt">design</span> exploration, for the concurrent generation of <span class="hlt">robust</span> system and subsystem specifications for the preliminary <span class="hlt">design</span> of multi-level, multi-objective, large-scale complex systems. This method is developed through the integration and expansion of current <span class="hlt">design</span> techniques: (1) Hierarchical partitioning and modeling techniques for partitioning large-scale complex systems into more tractable parts, and allowing integration of subproblems for system synthesis, (2) Statistical experimentation and approximation techniques for increasing both the efficiency and the comprehensiveness of preliminary <span class="hlt">design</span> exploration, and (3) Noise modeling techniques for implementing <span class="hlt">robust</span> preliminary <span class="hlt">design</span> when approximate models are employed. The method developed and associated approaches are illustrated through their application to the preliminary <span class="hlt">design</span> of a commercial turbofan turbine propulsion system; the turbofan system-level problem is partitioned into engine cycle and configuration <span class="hlt">design</span> and a compressor module is integrated for more detailed subsystem-level <span class="hlt">design</span> exploration, improving system evaluation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20090008513','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20090008513"><span>Reconfigurable Flight Control <span class="hlt">Design</span> using a <span class="hlt">Robust</span> Servo LQR and Radial Basis Function Neural Networks</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Burken, John J.</p> <p>2005-01-01</p> <p>This viewgraph presentation reviews the use of a <span class="hlt">Robust</span> Servo Linear Quadratic Regulator (LQR) and a Radial Basis Function (RBF) Neural Network in reconfigurable flight control <span class="hlt">designs</span> in adaptation to a aircraft part failure. The method uses a <span class="hlt">robust</span> LQR servomechanism <span class="hlt">design</span> with model Reference adaptive control, and RBF neural networks. During the failure the LQR servomechanism behaved well, and using the neural networks improved the tracking.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930000238&hterms=creating&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcreating','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930000238&hterms=creating&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcreating"><span>Creating A Data Base For <span class="hlt">Design</span> Of An Impeller</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Prueger, George H.; Chen, Wei-Chung</p> <p>1993-01-01</p> <p>Report describes use of <span class="hlt">Taguchi</span> method of parametric <span class="hlt">design</span> to create data base facilitating optimization of <span class="hlt">design</span> of impeller in centrifugal pump. Data base enables systematic <span class="hlt">design</span> analysis covering all significant <span class="hlt">design</span> parameters. Reduces time and cost of parametric optimization of <span class="hlt">design</span>: for particular impeller considered, one can cover 4,374 <span class="hlt">designs</span> by computational simulations of performance for only 18 cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017CRMec.345..712N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017CRMec.345..712N"><span>A hybrid multi-objective imperialist competitive algorithm and Monte Carlo method for <span class="hlt">robust</span> safety <span class="hlt">design</span> of a rail vehicle</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Nejlaoui, Mohamed; Houidi, Ajmi; Affi, Zouhaier; Romdhane, Lotfi</p> <p>2017-10-01</p> <p>This paper deals with the <span class="hlt">robust</span> safety <span class="hlt">design</span> optimization of a rail vehicle system moving in short radius curved tracks. A combined multi-objective imperialist competitive algorithm and Monte Carlo method is developed and used for the <span class="hlt">robust</span> multi-objective optimization of the rail vehicle system. This <span class="hlt">robust</span> optimization of rail vehicle safety considers simultaneously the derailment angle and its standard deviation where the <span class="hlt">design</span> parameters uncertainties are considered. The obtained results showed that the <span class="hlt">robust</span> <span class="hlt">design</span> reduces significantly the sensitivity of the rail vehicle safety to the <span class="hlt">design</span> parameters uncertainties compared to the determinist one and to the literature results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26999385','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26999385"><span>Optimal flexible sample size <span class="hlt">design</span> with <span class="hlt">robust</span> power.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zhang, Lanju; Cui, Lu; Yang, Bo</p> <p>2016-08-30</p> <p>It is well recognized that sample size determination is challenging because of the uncertainty on the treatment effect size. Several remedies are available in the literature. Group sequential <span class="hlt">designs</span> start with a sample size based on a conservative (smaller) effect size and allow early stop at interim looks. Sample size re-estimation <span class="hlt">designs</span> start with a sample size based on an optimistic (larger) effect size and allow sample size increase if the observed effect size is smaller than planned. Different opinions favoring one type over the other exist. We propose an optimal approach using an appropriate optimality criterion to select the best <span class="hlt">design</span> among all the candidate <span class="hlt">designs</span>. Our results show that (1) for the same type of <span class="hlt">designs</span>, for example, group sequential <span class="hlt">designs</span>, there is room for significant improvement through our optimization approach; (2) optimal promising zone <span class="hlt">designs</span> appear to have no advantages over optimal group sequential <span class="hlt">designs</span>; and (3) optimal <span class="hlt">designs</span> with sample size re-estimation deliver the best adaptive performance. We conclude that to deal with the challenge of sample size determination due to effect size uncertainty, an optimal approach can help to select the best <span class="hlt">design</span> that provides most <span class="hlt">robust</span> power across the effect size range of interest. Copyright © 2016 John Wiley & Sons, Ltd. Copyright © 2016 John Wiley & Sons, Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DPPBO4006H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DPPBO4006H"><span>Physics and <span class="hlt">Designs</span> of Ignition Capsules Using High-Density Carbon (HDC) Ablators: <span class="hlt">Robust</span> <span class="hlt">Designs</span>, Stability, and Shock Mergers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ho, D.; Salmonson, J.; Haan, S.; Clark, D.; Lindl, J.; Meezan, N.; Thomas, C.</p> <p>2015-11-01</p> <p>We present six ignition <span class="hlt">designs</span> using W-doped HDC ablators with, respectively, 2, 3, and 4-step increases in Tr. Fuel adiabat α ranges between 1.5 and 4. The 4-step <span class="hlt">design</span> has the lowest α of 1.5 but has the highest ablation front Rayleigh-Taylor (RT) growth. Consequently, the overall <span class="hlt">robustness</span> of the 4-step <span class="hlt">design</span> is inferior to the intermediate- α 3-step <span class="hlt">design</span>, assuming typical currently measured surface roughness spectrum. As the foot level is increased further and the shocks merge inside the fuel, the fuel adiabat is raised to 4. The RT growth and mix are reduced but the 1D margin is decreased making it overall more susceptible to surface roughness. The 2-step α = 2.5 <span class="hlt">design</span> turns out to be the most <span class="hlt">robust</span> against surface roughness and still can deliver very high 1D yield of 14.5 MJ. Systematic evaluation of the <span class="hlt">robustness</span> of these capsules with respect to low-mode radiation asymmetries, will also be discussed. Different paths to achieve low-convergence-ratio implosions (i.e. high velocity and high α as one option versus low velocity and low α as another option), while still giving respectable neutron yield will be presented. Finally, we discuss how the performance of these doped capsules changes; if the Au wall of the hohlraum is replaced by U. Work performed under auspices of U.S. DOE by LLNL under DE-AC52-07NA27344.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19910011334','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19910011334"><span>SSSFD manipulator engineering using statistical experiment <span class="hlt">design</span> techniques</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Barnes, John</p> <p>1991-01-01</p> <p>The Satellite Servicer System Flight Demonstration (SSSFD) program is a series of Shuttle flights <span class="hlt">designed</span> to verify major on-orbit satellite servicing capabilities, such as rendezvous and docking of free flyers, Orbital Replacement Unit (ORU) exchange, and fluid transfer. A major part of this system is the manipulator system that will perform the ORU exchange. The manipulator must possess adequate toolplate dexterity to maneuver a variety of EVA-type tools into position to interface with ORU fasteners, connectors, latches, and handles on the satellite, and to move workpieces and ORUs through 6 degree of freedom (dof) space from the Target Vehicle (TV) to the Support Module (SM) and back. Two cost efficient tools were combined to perform a study of robot manipulator <span class="hlt">design</span> parameters. These tools are graphical computer simulations and <span class="hlt">Taguchi</span> <span class="hlt">Design</span> of Experiment methods. Using a graphics platform, an off-the-shelf robot simulation software package, and an experiment <span class="hlt">designed</span> with <span class="hlt">Taguchi</span>'s approach, the sensitivities of various manipulator kinematic <span class="hlt">design</span> parameters to performance characteristics are determined with minimal cost.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ChJME..29..301J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ChJME..29..301J"><span><span class="hlt">Robust</span> <span class="hlt">design</span> optimization method for centrifugal impellers under surface roughness uncertainties due to blade fouling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ju, Yaping; Zhang, Chuhua</p> <p>2016-03-01</p> <p>Blade fouling has been proved to be a great threat to compressor performance in operating stage. The current researches on fouling-induced performance degradations of centrifugal compressors are based mainly on simplified roughness models without taking into account the realistic factors such as spatial non-uniformity and randomness of the fouling-induced surface roughness. Moreover, little attention has been paid to the <span class="hlt">robust</span> <span class="hlt">design</span> optimization of centrifugal compressor impellers with considerations of blade fouling. In this paper, a multi-objective <span class="hlt">robust</span> <span class="hlt">design</span> optimization method is developed for centrifugal impellers under surface roughness uncertainties due to blade fouling. A three-dimensional surface roughness map is proposed to describe the nonuniformity and randomness of realistic fouling accumulations on blades. To lower computational cost in <span class="hlt">robust</span> <span class="hlt">design</span> optimization, the support vector regression (SVR) metamodel is combined with the Monte Carlo simulation (MCS) method to conduct the uncertainty analysis of fouled impeller performance. The analyzed results show that the critical fouled region associated with impeller performance degradations lies at the leading edge of blade tip. The SVR metamodel has been proved to be an efficient and accurate means in the detection of impeller performance variations caused by roughness uncertainties. After <span class="hlt">design</span> optimization, the <span class="hlt">robust</span> optimal <span class="hlt">design</span> is found to be more efficient and less sensitive to fouling uncertainties while maintaining good impeller performance in the clean condition. This research proposes a systematic <span class="hlt">design</span> optimization method for centrifugal compressors with considerations of blade fouling, providing a practical guidance to the <span class="hlt">design</span> of advanced centrifugal compressors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000032558','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000032558"><span>Integration of the Response Surface Methodology with the Compromise Decision Support Problem in Developing a General <span class="hlt">Robust</span> <span class="hlt">Design</span> Procedure</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chen, Wei; Tsui, Kwok-Leung; Allen, Janet K.; Mistree, Farrokh</p> <p>1994-01-01</p> <p>In this paper we introduce a comprehensive and rigorous <span class="hlt">robust</span> <span class="hlt">design</span> procedure to overcome some limitations of the current approaches. A comprehensive approach is general enough to model the two major types of <span class="hlt">robust</span> <span class="hlt">design</span> applications, namely, <span class="hlt">robust</span> <span class="hlt">design</span> associated with the minimization of the deviation of performance caused by the deviation of noise factors (uncontrollable parameters), and <span class="hlt">robust</span> <span class="hlt">design</span> due to the minimization of the deviation of performance caused by the deviation of control factors (<span class="hlt">design</span> variables). We achieve mathematical rigor by using, as a foundation, principles from the <span class="hlt">design</span> of experiments and optimization. Specifically, we integrate the Response Surface Method (RSM) with the compromise Decision Support Problem (DSP). Our approach is especially useful for <span class="hlt">design</span> problems where there are no closed-form solutions and system performance is computationally expensive to evaluate. The <span class="hlt">design</span> of a solar powered irrigation system is used as an example. Our focus in this paper is on illustrating our approach rather than on the results per se.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1912060K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1912060K"><span><span class="hlt">Designing</span> Dynamic Adaptive Policy Pathways using Many-Objective <span class="hlt">Robust</span> Decision Making</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwakkel, Jan; Haasnoot, Marjolijn</p> <p>2017-04-01</p> <p>Dealing with climate risks in water management requires confronting a wide variety of deeply uncertain factors, while navigating a many dimensional space of trade-offs amongst objectives. There is an emerging body of literature on supporting this type of decision problem, under the label of decision making under deep uncertainty. Two approaches within this literature are Many-Objective <span class="hlt">Robust</span> Decision Making, and Dynamic Adaptive Policy Pathways. In recent work, these approaches have been compared. One of the main conclusions of this comparison was that they are highly complementary. Many-Objective <span class="hlt">Robust</span> Decision Making is a model based decision support approach, while Dynamic Adaptive Policy Pathways is primarily a conceptual framework for the <span class="hlt">design</span> of flexible strategies that can be adapted over time in response to how the future is actually unfolding. In this research we explore this complementarity in more detail. Specifically, we demonstrate how Many-Objective <span class="hlt">Robust</span> Decision Making can be used to <span class="hlt">design</span> adaptation pathways. We demonstrate this combined approach using a water management problem, in the Netherlands. The water level of Lake IJselmeer, the main fresh water resource of the Netherlands, is currently managed through discharge by gravity. Due to climate change, this won't be possible in the future, unless water levels are changed. Changing the water level has undesirable flood risk and spatial planning consequences. The challenge is to find promising adaptation pathways that balance objectives related to fresh water supply, flood risk, and spatial issues, while accounting for uncertain climatic and land use change. We conclude that the combination of Many-Objective <span class="hlt">Robust</span> Decision Making and Dynamic Adaptive Policy Pathways is particularly suited for dealing with deeply uncertain climate risks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2001PhDT........25I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2001PhDT........25I"><span><span class="hlt">Robust</span> dynamic inversion controller <span class="hlt">design</span> and analysis (using the X-38 vehicle as a case study)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ito, Daigoro</p> <p></p> <p>A new way to approach <span class="hlt">robust</span> Dynamic Inversion controller synthesis is addressed in this paper. A Linear Quadratic Gaussian outer-loop controller improves the <span class="hlt">robustness</span> of a Dynamic Inversion inner-loop controller in the presence of uncertainties. Desired dynamics are given by the dynamic compensator, which shapes the loop. The selected dynamics are based on both performance and stability <span class="hlt">robustness</span> requirements. These requirements are straightforwardly formulated as frequency-dependent singular value bounds during synthesis of the controller. Performance and <span class="hlt">robustness</span> of the <span class="hlt">designed</span> controller is tested using a worst case time domain quadratic index, which is a simple but effective way to measure <span class="hlt">robustness</span> due to parameter variation. Using this approach, a lateral-directional controller for the X-38 vehicle is <span class="hlt">designed</span> and its <span class="hlt">robustness</span> to parameter variations and disturbances is analyzed. It is found that if full state measurements are available, the performance of the <span class="hlt">designed</span> lateral-directional control system, measured by the chosen cost function, improves by approximately a factor of four. Also, it is found that the <span class="hlt">designed</span> system is stable up to a parametric variation of 1.65 standard deviation with the set of uncertainty considered. The system <span class="hlt">robustness</span> is determined to be highly sensitive to the dihedral derivative and the roll damping coefficients. The controller analysis is extended to the nonlinear system where both control input displacements and rates are bounded. In this case, the considered nonlinear system is stable up to 48.1° in bank angle and 1.59° in sideslip angle variations, indicating it is more sensitive to variations in sideslip angle than in bank angle. This nonlinear approach is further extended for the actuator failure mode analysis. The results suggest that the <span class="hlt">designed</span> system maintains a high level of stability in the event of aileron failure. However, only 35% or less of the original stability range is maintained for the</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_11 --> <div id="page_12" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="221"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015EGUGA..17.8937K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015EGUGA..17.8937K"><span>How <span class="hlt">robust</span> is a <span class="hlt">robust</span> policy? A comparative analysis of alternative <span class="hlt">robustness</span> metrics for supporting <span class="hlt">robust</span> decision analysis.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwakkel, Jan; Haasnoot, Marjolijn</p> <p>2015-04-01</p> <p>In response to climate and socio-economic change, in various policy domains there is increasingly a call for <span class="hlt">robust</span> plans or policies. That is, plans or policies that performs well in a very large range of plausible futures. In the literature, a wide range of alternative <span class="hlt">robustness</span> metrics can be found. The relative merit of these alternative conceptualizations of <span class="hlt">robustness</span> has, however, received less attention. Evidently, different <span class="hlt">robustness</span> metrics can result in different plans or policies being adopted. This paper investigates the consequences of several <span class="hlt">robustness</span> metrics on decision making, illustrated here by the <span class="hlt">design</span> of a flood risk management plan. A fictitious case, inspired by a river reach in the Netherlands is used. The performance of this system in terms of casualties, damages, and costs for flood and damage mitigation actions is explored using a time horizon of 100 years, and accounting for uncertainties pertaining to climate change and land use change. A set of candidate policy options is specified up front. This set of options includes dike raising, dike strengthening, creating more space for the river, and flood proof building and evacuation options. The overarching aim is to <span class="hlt">design</span> an effective flood risk mitigation strategy that is <span class="hlt">designed</span> from the outset to be adapted over time in response to how the future actually unfolds. To this end, the plan will be based on the dynamic adaptive policy pathway approach (Haasnoot, Kwakkel et al. 2013) being used in the Dutch Delta Program. The policy problem is formulated as a multi-objective <span class="hlt">robust</span> optimization problem (Kwakkel, Haasnoot et al. 2014). We solve the multi-objective <span class="hlt">robust</span> optimization problem using several alternative <span class="hlt">robustness</span> metrics, including both satisficing <span class="hlt">robustness</span> metrics and regret based <span class="hlt">robustness</span> metrics. Satisficing <span class="hlt">robustness</span> metrics focus on the performance of candidate plans across a large ensemble of plausible futures. Regret based <span class="hlt">robustness</span> metrics compare the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MeScT..28d5405M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MeScT..28d5405M"><span><span class="hlt">Robust</span> surface reconstruction by <span class="hlt">design</span>-guided SEM photometric stereo</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Miyamoto, Atsushi; Matsuse, Hiroki; Koutaki, Gou</p> <p>2017-04-01</p> <p>We present a novel approach that addresses the blind reconstruction problem in scanning electron microscope (SEM) photometric stereo for complicated semiconductor patterns to be measured. In our previous work, we developed a bootstrapping de-shadowing and self-calibration (BDS) method, which automatically calibrates the parameter of the gradient measurement formulas and resolves shadowing errors for estimating an accurate three-dimensional (3D) shape and underlying shadowless images. Experimental results on 3D surface reconstruction demonstrated the significance of the BDS method for simple shapes, such as an isolated line pattern. However, we found that complicated shapes, such as line-and-space (L&S) and multilayered patterns, produce deformed and inaccurate measurement results. This problem is due to brightness fluctuations in the SEM images, which are mainly caused by the energy fluctuations of the primary electron beam, variations in the electronic expanse inside a specimen, and electrical charging of specimens. Despite these being essential difficulties encountered in SEM photometric stereo, it is difficult to model accurately all the complicated physical phenomena of electronic behavior. We improved the <span class="hlt">robustness</span> of the surface reconstruction in order to deal with these practical difficulties with complicated shapes. Here, <span class="hlt">design</span> data are useful clues as to the pattern layout and layer information of integrated semiconductors. We used the <span class="hlt">design</span> data as a guide of the measured shape and incorporated a geometrical constraint term to evaluate the difference between the measured and <span class="hlt">designed</span> shapes into the objective function of the BDS method. Because the true shape does not necessarily correspond to the <span class="hlt">designed</span> one, we use an iterative scheme to develop proper guide patterns and a 3D surface that provides both a less distorted and more accurate 3D shape after convergence. Extensive experiments on real image data demonstrate the <span class="hlt">robustness</span> and effectiveness</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23006066','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23006066"><span>Estimating open population site occupancy from presence-absence data lacking the <span class="hlt">robust</span> <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dail, D; Madsen, L</p> <p>2013-03-01</p> <p>Many animal monitoring studies seek to estimate the proportion of a study area occupied by a target population. The study area is divided into spatially distinct sites where the detected presence or absence of the population is recorded, and this is repeated in time for multiple seasons. However, when occupied sites are detected with probability p < 1, the lack of a detection does not imply lack of occupancy. MacKenzie et al. (2003, Ecology 84, 2200-2207) developed a multiseason model for estimating seasonal site occupancy (ψt ) while accounting for unknown p. Their model performs well when observations are collected according to the <span class="hlt">robust</span> <span class="hlt">design</span>, where multiple sampling occasions occur during each season; the repeated sampling aids in the estimation p. However, their model does not perform as well when the <span class="hlt">robust</span> <span class="hlt">design</span> is lacking. In this paper, we propose an alternative likelihood model that yields improved seasonal estimates of p and Ψt in the absence of the <span class="hlt">robust</span> <span class="hlt">design</span>. We construct the marginal likelihood of the observed data by conditioning on, and summing out, the latent number of occupied sites during each season. A simulation study shows that in cases without the <span class="hlt">robust</span> <span class="hlt">design</span>, the proposed model estimates p with less bias than the MacKenzie et al. model and hence improves the estimates of Ψt . We apply both models to a data set consisting of repeated presence-absence observations of American robins (Turdus migratorius) with yearly survey periods. The two models are compared to a third estimator available when the repeated counts (from the same study) are considered, with the proposed model yielding estimates of Ψt closest to estimates from the point count model. Copyright © 2013, The International Biometric Society.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19810011295','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19810011295"><span>Preliminary demonstration of a <span class="hlt">robust</span> controller <span class="hlt">design</span> method</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Anderson, L. R.</p> <p>1980-01-01</p> <p>Alternative computational procedures for obtaining a feedback control law which yields a control signal based on measurable quantitites are evaluated. The three methods evaluated are: (1) the standard linear quadratic regulator <span class="hlt">design</span> model; (2) minimization of the norm of the feedback matrix, k via nonlinear programming subject to the constraint that the closed loop eigenvalues be in a specified domain in the complex plane; and (3) maximize the angles between the closed loop eigenvectors in combination with minimizing the norm of K also via the constrained nonlinear programming. The third or <span class="hlt">robust</span> <span class="hlt">design</span> method was chosen to yield a closed loop system whose eigenvalues are insensitive to small changes in the A and B matrices. The relationship between orthogonality of closed loop eigenvectors and the sensitivity of closed loop eigenvalues is described. Computer programs are described.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016IJTJE..33..275R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016IJTJE..33..275R"><span><span class="hlt">Taguchi</span> Based Regression Analysis of End-Wall Film Cooling in a Gas Turbine Cascade with Single Row of Holes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ravi, D.; Parammasivam, K. M.</p> <p>2016-09-01</p> <p>Numerical investigations were conducted on a turbine cascade, with end-wall cooling by a single row of cylindrical holes, inclined at 30°. The mainstream fluid was hot air and the coolant was CO2 gas. Based on the Reynolds number, the flow was turbulent at the inlet. The film hole row position, its pitch and blowing ratio was varied with five different values. <span class="hlt">Taguchi</span> approach was used in <span class="hlt">designing</span> a L25 orthogonal array (OA) for these parameters. The end-wall averaged film cooling effectiveness (bar η) was chosen as the quality characteristic. CFD analyses were carried out using Ansys Fluent on computational domains <span class="hlt">designed</span> with inputs from OA. Experiments were conducted for one chosen OA configuration and the computational results were found to correlate well with experimental measurements. The responses from the CFD analyses were fed to the statistical tool to develop a correlation for bar η using regression analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015IJMPC..2650024P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015IJMPC..2650024P"><span>Efficiency and <span class="hlt">robustness</span> of different bus network <span class="hlt">designs</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pang, John Zhen Fu; Bin Othman, Nasri; Ng, Keng Meng; Monterola, Christopher</p> <p>2015-07-01</p> <p>We compare the efficiencies and <span class="hlt">robustness</span> of four transport networks that can be possibly formed as a result of deliberate city planning. The networks are constructed based on their spatial resemblance to the cities of Manhattan (lattice), Sudan (random), Beijing (single-blob) and Greater Cairo (dual-blob). For a given type, a genetic algorithm is employed to obtain an optimized set of the bus routes. We then simulate how commuter travels using Yen's algorithms for k shortest paths on an adjacency matrix. The cost of traveling such as walking between stations is captured by varying the weighted sums of matrices. We also consider the number of transfers a posteriori by looking at the computed shortest paths. With consideration to distances via radius of gyration, redundancies of travel and number of bus transfers, our simulations indicate that random and dual-blob are more efficient than single-blob and lattice networks. Moreover, dual-blob type is least <span class="hlt">robust</span> when node removals are targeted but is most resilient when node failures are random. The work hopes to guide and provide technical perspectives on how geospatial distribution of a city limits the optimality of transport <span class="hlt">designs</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016IJC....89.2201K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016IJC....89.2201K"><span><span class="hlt">Design</span> and experimental evaluation of <span class="hlt">robust</span> controllers for a two-wheeled robot</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kralev, J.; Slavov, Ts.; Petkov, P.</p> <p>2016-11-01</p> <p>The paper presents the <span class="hlt">design</span> and experimental evaluation of two alternative μ-controllers for <span class="hlt">robust</span> vertical stabilisation of a two-wheeled self-balancing robot. The controllers <span class="hlt">design</span> is based on models derived by identification from closed-loop experimental data. In the first <span class="hlt">design</span>, a signal-based uncertainty representation obtained directly from the identification procedure is used, which leads to a controller of order 29. In the second <span class="hlt">design</span> the signal uncertainty is approximated by an input multiplicative uncertainty, which leads to a controller of order 50, subsequently reduced to 30. The performance of the two μ-controllers is compared with the performance of a conventional linear quadratic controller with 17th-order Kalman filter. A proportional-integral controller of the rotational motion around the vertical axis is implemented as well. The control code is generated using Simulink® controller models and is embedded in a digital signal processor. Results from the simulation of the closed-loop system as well as experimental results obtained during the real-time implementation of the <span class="hlt">designed</span> controllers are given. The theoretical investigation and experimental results confirm that the closed-loop system achieves <span class="hlt">robust</span> performance in respect to the uncertainties related to the identified robot model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23618744','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23618744"><span><span class="hlt">Robust</span> attitude control <span class="hlt">design</span> for spacecraft under assigned velocity and control constraints.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hu, Qinglei; Li, Bo; Zhang, Youmin</p> <p>2013-07-01</p> <p>A novel <span class="hlt">robust</span> nonlinear control <span class="hlt">design</span> under the constraints of assigned velocity and actuator torque is investigated for attitude stabilization of a rigid spacecraft. More specifically, a nonlinear feedback control is firstly developed by explicitly taking into account the constraints on individual angular velocity components as well as external disturbances. Considering further the actuator misalignments and magnitude deviation, a modified <span class="hlt">robust</span> least-squares based control allocator is employed to deal with the problem of distributing the previously <span class="hlt">designed</span> three-axis moments over the available actuators, in which the focus of this control allocation is to find the optimal control vector of actuators by minimizing the worst-case residual error using programming algorithms. The attitude control performance using the controller structure is evaluated through a numerical example. Copyright © 2013 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15520792','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15520792"><span>Biological <span class="hlt">robustness</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kitano, Hiroaki</p> <p>2004-11-01</p> <p><span class="hlt">Robustness</span> is a ubiquitously observed property of biological systems. It is considered to be a fundamental feature of complex evolvable systems. It is attained by several underlying principles that are universal to both biological organisms and sophisticated engineering systems. <span class="hlt">Robustness</span> facilitates evolvability and <span class="hlt">robust</span> traits are often selected by evolution. Such a mutually beneficial process is made possible by specific architectural features observed in <span class="hlt">robust</span> systems. But there are trade-offs between <span class="hlt">robustness</span>, fragility, performance and resource demands, which explain system behaviour, including the patterns of failure. Insights into inherent properties of <span class="hlt">robust</span> systems will provide us with a better understanding of complex diseases and a guiding principle for therapy <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EPJWC.16201003M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EPJWC.16201003M"><span>Optimization of reactive-ion etching (RIE) parameters for fabrication of tantalum pentoxide (Ta2O5) waveguide using <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Muttalib, M. Firdaus A.; Chen, Ruiqi Y.; Pearce, S. J.; Charlton, Martin D. B.</p> <p>2017-11-01</p> <p>In this paper, we demonstrate the optimization of reactive-ion etching (RIE) parameters for the fabrication of tantalum pentoxide (Ta2O5) waveguide with chromium (Cr) hard mask in a commercial OIPT Plasmalab 80 RIE etcher. A <span class="hlt">design</span> of experiment (DOE) using <span class="hlt">Taguchi</span> method was implemented to find optimum RF power, mixture of CHF3 and Ar gas ratio, and chamber pressure for a high etch rate, good selectivity, and smooth waveguide sidewall. It was found that the optimized etch condition obtained in this work were RF power = 200 W, gas ratio = 80 %, and chamber pressure = 30 mTorr with an etch rate of 21.6 nm/min, Ta2O5/Cr selectivity ratio of 28, and smooth waveguide sidewall.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..MARB44012L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..MARB44012L"><span>Hiding the weakness: structural <span class="hlt">robustness</span> using origami <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Bin; Santangelo, Christian; Cohen, Itai</p> <p>2015-03-01</p> <p>A non-deformable structure is typically associated with infinitely stiff materials that resist distortion. In this work, we <span class="hlt">designed</span> a structure with a region that will not deform even though it is made of arbitrarily compliant materials. More specifically, we show that a foldable sheet with a circular hole in the middle can be deformed externally with the internal geometry of the hole unaffected. Instead of strengthening the local stiffness, we fine tune the crease patterns so that all the soft modes that can potentially deform the internal geometry are not accessible through strain on the external boundary. The inner structure is thus protected by the topological mechanics, based on the detailed geometry of how the vertices in the foldable sheet are connected. In this way, we isolate the structural <span class="hlt">robustness</span> from the mechanical properties of the materials, which introduces an extra degree of freedom for structural <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000097938','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000097938"><span><span class="hlt">Robust</span> Fixed-Structure Controller Synthesis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Corrado, Joseph R.; Haddad, Wassim M.; Gupta, Kajal (Technical Monitor)</p> <p>2000-01-01</p> <p>The ability to develop an integrated control system <span class="hlt">design</span> methodology for <span class="hlt">robust</span> high performance controllers satisfying multiple <span class="hlt">design</span> criteria and real world hardware constraints constitutes a challenging task. The increasingly stringent performance specifications required for controlling such systems necessitates a trade-off between controller complexity and <span class="hlt">robustness</span>. The principle challenge of the minimal complexity <span class="hlt">robust</span> control <span class="hlt">design</span> is to arrive at a tractable control <span class="hlt">design</span> formulation in spite of the extreme complexity of such systems. Hence, <span class="hlt">design</span> of minimal complexitY <span class="hlt">robust</span> controllers for systems in the face of modeling errors has been a major preoccupation of system and control theorists and practitioners for the past several decades.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013MatSP..31..424P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013MatSP..31..424P"><span>Optimization of sol-gel technique for coating of metallic substrates by hydroxyapatite using the <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pourbaghi-Masouleh, M.; Asgharzadeh, H.</p> <p>2013-08-01</p> <p>In this study, the <span class="hlt">Taguchi</span> method of <span class="hlt">design</span> of experiment (DOE) was used to optimize the hydroxyapatite (HA) coatings on various metallic substrates deposited by sol-gel dip-coating technique. The experimental <span class="hlt">design</span> consisted of five factors including substrate material (A), surface preparation of substrate (B), dipping/withdrawal speed (C), number of layers (D), and calcination temperature (E) with three levels of each factor. An orthogonal array of L18 type with mixed levels of the control factors was utilized. The image processing of the micrographs of the coatings was conducted to determine the percentage of coated area ( PCA). Chemical and phase composition of HA coatings were studied by XRD, FT-IR, SEM, and EDS techniques. The analysis of variance (ANOVA) indicated that the PCA of HA coatings was significantly affected by the calcination temperature. The optimum conditions from signal-to-noise ( S/N) ratio analysis were A: pure Ti, B: polishing and etching for 24 h, C: 50 cm min-1, D: 1, and E: 300 °C. In the confirmation experiment using the optimum conditions, the HA coating with high PCA of 98.5 % was obtained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930053007&hterms=feedforward+control&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dfeedforward%2Bcontrol','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930053007&hterms=feedforward+control&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dfeedforward%2Bcontrol"><span><span class="hlt">Design</span> and evaluation of a <span class="hlt">robust</span> dynamic neurocontroller for a multivariable aircraft control problem</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Troudet, T.; Garg, S.; Merrill, W.</p> <p>1992-01-01</p> <p>The <span class="hlt">design</span> of a dynamic neurocontroller with good <span class="hlt">robustness</span> properties is presented for a multivariable aircraft control problem. The internal dynamics of the neurocontroller are synthesized by a state estimator feedback loop. The neurocontrol is generated by a multilayer feedforward neural network which is trained through backpropagation to minimize an objective function that is a weighted sum of tracking errors, and control input commands and rates. The neurocontroller exhibits good <span class="hlt">robustness</span> through stability margins in phase and vehicle output gains. By maintaining performance and stability in the presence of sensor failures in the error loops, the structure of the neurocontroller is also consistent with the classical approach of flight control <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017SPIE10445E..5GK','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017SPIE10445E..5GK"><span>Application of <span class="hlt">Taguchi</span> method to optimization of surface roughness during precise turning of NiTi shape memory alloy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kowalczyk, M.</p> <p>2017-08-01</p> <p>This paper describes the research results of surface quality research after the NiTi shape memory alloy (Nitinol) precise turning by the tools with edges made of polycrystalline diamonds (PCD). Nitinol, a nearly equiatomic nickel-titanium shape memory alloy, has wide applications in the arms industry, military, medicine and aerospace industry, and industrial robots. Due to their specific properties NiTi alloys are known to be difficult-to-machine materials particularly by using conventional techniques. The research trials were conducted for three independent parameters (vc, f, ap) affecting the surface roughness were analyzed. The choice of parameter configurations were performed by factorial <span class="hlt">design</span> methods using orthogonal plan type L9, with three control factors, changing on three levels, developed by G. <span class="hlt">Taguchi</span>. S/N ratio and ANOVA analyses were performed to identify the best of cutting parameters influencing surface roughness.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20070010767','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20070010767"><span><span class="hlt">Robust</span> Constrained Optimization Approach to Control <span class="hlt">Design</span> for International Space Station Centrifuge Rotor Auto Balancing Control System</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Postma, Barry Dirk</p> <p>2005-01-01</p> <p>This thesis discusses application of a <span class="hlt">robust</span> constrained optimization approach to control <span class="hlt">design</span> to develop an Auto Balancing Controller (ABC) for a centrifuge rotor to be implemented on the International Space Station. The <span class="hlt">design</span> goal is to minimize a performance objective of the system, while guaranteeing stability and proper performance for a range of uncertain plants. The Performance objective is to minimize the translational response of the centrifuge rotor due to a fixed worst-case rotor imbalance. The <span class="hlt">robustness</span> constraints are posed with respect to parametric uncertainty in the plant. The proposed approach to control <span class="hlt">design</span> allows for both of these objectives to be handled within the framework of constrained optimization. The resulting controller achieves acceptable performance and <span class="hlt">robustness</span> characteristics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960027527','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960027527"><span>A <span class="hlt">robust</span> rotorcraft flight control system <span class="hlt">design</span> methodology utilizing quantitative feedback theory</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gorder, Peter James</p> <p>1993-01-01</p> <p>Rotorcraft flight control systems present <span class="hlt">design</span> challenges which often exceed those associated with fixed-wing aircraft. First, large variations in the response characteristics of the rotorcraft result from the wide range of airspeeds of typical operation (hover to over 100 kts). Second, the assumption of vehicle rigidity often employed in the <span class="hlt">design</span> of fixed-wing flight control systems is rarely justified in rotorcraft where rotor degrees of freedom can have a significant impact on the system performance and stability. This research was intended to develop a methodology for the <span class="hlt">design</span> of <span class="hlt">robust</span> rotorcraft flight control systems. Quantitative Feedback Theory (QFT) was chosen as the basis for the investigation. Quantitative Feedback Theory is a technique which accounts for variability in the dynamic response of the controlled element in the <span class="hlt">design</span> <span class="hlt">robust</span> control systems. It was developed to address a Multiple-Input Single-Output (MISO) <span class="hlt">design</span> problem, and utilizes two degrees of freedom to satisfy the <span class="hlt">design</span> criteria. Two techniques were examined for extending the QFT MISO technique to the <span class="hlt">design</span> of a Multiple-Input-Multiple-Output (MIMO) flight control system (FCS) for a UH-60 Black Hawk Helicopter. In the first, a set of MISO systems, mathematically equivalent to the MIMO system, was determined. QFT was applied to each member of the set simultaneously. In the second, the same set of equivalent MISO systems were analyzed sequentially, with closed loop response information from each loop utilized in subsequent MISO <span class="hlt">designs</span>. The results of each technique were compared, and the advantages of the second, termed Sequential Loop Closure, were clearly evident.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AIPC.1952b0058K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AIPC.1952b0058K"><span>Optimization the mechanical properties of coir-luffa cylindrica filled hybrid composites by using <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Krishnudu, D. Mohana; Sreeramulu, D.; Reddy, P. Venkateshwar</p> <p>2018-04-01</p> <p>In the current study mechanical properties of particles filled hybrid composites have been studied. The mechanical properties of the hybrid composite mainly depend on the proportions of the coir weight, Luffa weight and filler weight. RSM along with <span class="hlt">Taguchi</span> method have been applied to find the optimized parameters of the hybrid composites. From the current study it was observed that the tensile strength of the composite mainly depends on the coir percent than the other two particles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030068106','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030068106"><span><span class="hlt">Robust</span> Control for Microgravity Vibration Isolation using Fixed Order, Mixed H2/Mu <span class="hlt">Design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Whorton, Mark</p> <p>2003-01-01</p> <p>Many space-science experiments need an active isolation system to provide a sufficiently quiescent microgravity environment. Modern control methods provide the potential for both high-performance and <span class="hlt">robust</span> stability in the presence of parametric uncertainties that are characteristic of microgravity vibration isolation systems. While H2 and H(infinity) methods are well established, neither provides the levels of attenuation performance and <span class="hlt">robust</span> stability in a compensator with low order. Mixed H2/H(infinity), controllers provide a means for maximizing <span class="hlt">robust</span> stability for a given level of mean-square nominal performance while directly optimizing for controller order constraints. This paper demonstrates the benefit of mixed norm <span class="hlt">design</span> from the perspective of <span class="hlt">robustness</span> to parametric uncertainties and controller order for microgravity vibration isolation. A nominal performance metric analogous to the mu measure, for <span class="hlt">robust</span> stability assessment is also introduced in order to define an acceptable trade space from which different control methodologies can be compared.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930046901&hterms=desensitization&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Ddesensitization','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930046901&hterms=desensitization&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Ddesensitization"><span><span class="hlt">Robustness</span>. [in space systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ryan, Robert</p> <p>1993-01-01</p> <p>The concept of rubustness includes <span class="hlt">design</span> simplicity, component and path redundancy, desensitization to the parameter and environment variations, control of parameter variations, and punctual operations. These characteristics must be traded with functional concepts, materials, and fabrication approach against the criteria of performance, cost, and reliability. The paper describes the <span class="hlt">robustness</span> <span class="hlt">design</span> process, which includes the following seven major coherent steps: translation of vision into requirements, definition of the <span class="hlt">robustness</span> characteristics desired, criteria formulation of required <span class="hlt">robustness</span>, concept selection, detail <span class="hlt">design</span>, manufacturing and verification, operations.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_12 --> <div id="page_13" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="241"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007PhDT........77D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007PhDT........77D"><span><span class="hlt">Robust</span> parameter <span class="hlt">design</span> for automatically controlled systems and nanostructure synthesis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dasgupta, Tirthankar</p> <p>2007-12-01</p> <p>This research focuses on developing comprehensive frameworks for developing <span class="hlt">robust</span> parameter <span class="hlt">design</span> methodology for dynamic systems with automatic control and for synthesis of nanostructures. In many automatically controlled dynamic processes, the optimal feedback control law depends on the parameter <span class="hlt">design</span> solution and vice versa and therefore an integrated approach is necessary. A parameter <span class="hlt">design</span> methodology in the presence of feedback control is developed for processes of long duration under the assumption that experimental noise factors are uncorrelated over time. Systems that follow a pure-gain dynamic model are considered and the best proportional-integral and minimum mean squared error control strategies are developed by using <span class="hlt">robust</span> parameter <span class="hlt">design</span>. The proposed method is illustrated using a simulated example and a case study in a urea packing plant. This idea is also extended to cases with on-line noise factors. The possibility of integrating feedforward control with a minimum mean squared error feedback control scheme is explored. To meet the needs of large scale synthesis of nanostructures, it is critical to systematically find experimental conditions under which the desired nanostructures are synthesized reproducibly, at large quantity and with controlled morphology. The first part of the research in this area focuses on modeling and optimization of existing experimental data. Through a rigorous statistical analysis of experimental data, models linking the probabilities of obtaining specific morphologies to the process variables are developed. A new iterative algorithm for fitting a Multinomial GLM is proposed and used. The optimum process conditions, which maximize the above probabilities and make the synthesis process less sensitive to variations of process variables around set values, are derived from the fitted models using Monte-Carlo simulations. The second part of the research deals with development of an experimental <span class="hlt">design</span> methodology, tailor</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150005708','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150005708"><span><span class="hlt">Robust</span> Stability Analysis of the Space Launch System Control <span class="hlt">Design</span>: A Singular Value Approach</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Pei, Jing; Newsome, Jerry R.</p> <p>2015-01-01</p> <p>Classical stability analysis consists of breaking the feedback loops one at a time and determining separately how much gain or phase variations would destabilize the stable nominal feedback system. For typical launch vehicle control <span class="hlt">design</span>, classical control techniques are generally employed. In addition to stability margins, frequency domain Monte Carlo methods are used to evaluate the <span class="hlt">robustness</span> of the <span class="hlt">design</span>. However, such techniques were developed for Single-Input-Single-Output (SISO) systems and do not take into consideration the off-diagonal terms in the transfer function matrix of Multi-Input-Multi-Output (MIMO) systems. <span class="hlt">Robust</span> stability analysis techniques such as H(sub infinity) and mu are applicable to MIMO systems but have not been adopted as standard practices within the launch vehicle controls community. This paper took advantage of a simple singular-value-based MIMO stability margin evaluation method based on work done by Mukhopadhyay and Newsom and applied it to the SLS high-fidelity dynamics model. The method computes a simultaneous multi-loop gain and phase margin that could be related back to classical margins. The results presented in this paper suggest that for the SLS system, traditional SISO stability margins are similar to the MIMO margins. This additional level of verification provides confidence in the <span class="hlt">robustness</span> of the control <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930018985','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930018985"><span><span class="hlt">Robust</span> control for uncertain structures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Douglas, Joel; Athans, Michael</p> <p>1991-01-01</p> <p>Viewgraphs on <span class="hlt">robust</span> control for uncertain structures are presented. Topics covered include: <span class="hlt">robust</span> linear quadratic regulator (RLQR) formulas; mismatched LQR <span class="hlt">design</span>; RLQR <span class="hlt">design</span>; interpretations of RLQR <span class="hlt">design</span>; disturbance rejection; and performance comparisons: RLQR vs. mismatched LQR.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20806254','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20806254"><span>Optimization of laccase production by Pleurotus ostreatus IMI 395545 using the <span class="hlt">Taguchi</span> DOE methodology.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Periasamy, Rathinasamy; Palvannan, Thayumanavan</p> <p>2010-12-01</p> <p>Production of laccase using a submerged culture of Pleurotus orstreatus IMI 395545 was optimized by the <span class="hlt">Taguchi</span> orthogonal array (OA) <span class="hlt">design</span> of experiments (DOE) methodology. This approach facilitates the study of the interactions of a large number of variables spanned by factors and their settings, with a small number of experiments, leading to considerable savings in time and cost for process optimization. This methodology optimizes the number of impact factors and enables to calculate their interaction in the production of industrial enzymes. Eight factors, viz. glucose, yeast extract, malt extract, inoculum, mineral solution, inducer (1 mM CuSO₄) and amino acid (l-asparagine) at three levels and pH at two levels, with an OA layout of L18 (2¹ × 3⁷) were selected for the proposed experimental <span class="hlt">design</span>. The laccase yield obtained from the 18 sets of fermentation experiments performed with the selected factors and levels was further processed with Qualitek-4 software. The optimized conditions shared an enhanced laccase expression of 86.8% (from 485.0 to 906.3 U). The combination of factors was further validated for laccase production and reactive blue 221 decolorization. The results revealed an enhanced laccase yield of 32.6% and dye decolorization up to 84.6%. This methodology allows the complete evaluation of main and interaction factors. © 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5320970','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5320970"><span><span class="hlt">Design</span> principles for <span class="hlt">robust</span> vesiculation in clathrin-mediated endocytosis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Hassinger, Julian E.; Oster, George; Drubin, David G.; Rangamani, Padmini</p> <p>2017-01-01</p> <p>A critical step in cellular-trafficking pathways is the budding of membranes by protein coats, which recent experiments have demonstrated can be inhibited by elevated membrane tension. The <span class="hlt">robustness</span> of processes like clathrin-mediated endocytosis (CME) across a diverse range of organisms and mechanical environments suggests that the protein machinery in this process has evolved to take advantage of some set of physical <span class="hlt">design</span> principles to ensure <span class="hlt">robust</span> vesiculation against opposing forces like membrane tension. Using a theoretical model for membrane mechanics and membrane protein interaction, we have systematically investigated the influence of membrane rigidity, curvature induced by the protein coat, area covered by the protein coat, membrane tension, and force from actin polymerization on bud formation. Under low tension, the membrane smoothly evolves from a flat to budded morphology as the coat area or spontaneous curvature increases, whereas the membrane remains essentially flat at high tensions. At intermediate, physiologically relevant, tensions, the membrane undergoes a “snap-through instability” in which small changes in the coat area, spontaneous curvature or membrane tension cause the membrane to “snap” from an open, U-shape to a closed bud. This instability can be smoothed out by increasing the bending rigidity of the coat, allowing for successful budding at higher membrane tensions. Additionally, applied force from actin polymerization can bypass the instability by inducing a smooth transition from an open to a closed bud. Finally, a combination of increased coat rigidity and force from actin polymerization enables <span class="hlt">robust</span> vesiculation even at high membrane tensions. PMID:28126722</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970004929','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970004929"><span>Multi-Criterion Preliminary <span class="hlt">Design</span> of a Tetrahedral Truss Platform</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wu, K. Chauncey</p> <p>1995-01-01</p> <p>An efficient method is presented for multi-criterion preliminary <span class="hlt">design</span> and demonstrated for a tetrahedral truss platform. The present method requires minimal analysis effort and permits rapid estimation of optimized truss behavior for preliminary <span class="hlt">design</span>. A 14-m-diameter, 3-ring truss platform represents a candidate reflector support structure for space-based science spacecraft. The truss members are divided into 9 groups by truss ring and position. <span class="hlt">Design</span> variables are the cross-sectional area of all members in a group, and are either 1, 3 or 5 times the minimum member area. Non-structural mass represents the node and joint hardware used to assemble the truss structure. <span class="hlt">Taguchi</span> methods are used to efficiently identify key points in the set of Pareto-optimal truss <span class="hlt">designs</span>. Key points identified using <span class="hlt">Taguchi</span> methods are the maximum frequency, minimum mass, and maximum frequency-to-mass ratio truss <span class="hlt">designs</span>. Low-order polynomial curve fits through these points are used to approximate the behavior of the full set of Pareto-optimal <span class="hlt">designs</span>. The resulting Pareto-optimal <span class="hlt">design</span> curve is used to predict frequency and mass for optimized trusses. Performance improvements are plotted in frequency-mass (criterion) space and compared to results for uniform trusses. Application of constraints to frequency and mass and sensitivity to constraint variation are demonstrated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JIEIC..98..607K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JIEIC..98..607K"><span>Optimization of Surface Roughness Parameters of Al-6351 Alloy in EDC Process: A <span class="hlt">Taguchi</span> Coupled Fuzzy Logic Approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kar, Siddhartha; Chakraborty, Sujoy; Dey, Vidyut; Ghosh, Subrata Kumar</p> <p>2017-10-01</p> <p>This paper investigates the application of <span class="hlt">Taguchi</span> method with fuzzy logic for multi objective optimization of roughness parameters in electro discharge coating process of Al-6351 alloy with powder metallurgical compacted SiC/Cu tool. A <span class="hlt">Taguchi</span> L16 orthogonal array was employed to investigate the roughness parameters by varying tool parameters like composition and compaction load and electro discharge machining parameters like pulse-on time and peak current. Crucial roughness parameters like Centre line average roughness, Average maximum height of the profile and Mean spacing of local peaks of the profile were measured on the coated specimen. The signal to noise ratios were fuzzified to optimize the roughness parameters through a single comprehensive output measure (COM). Best COM obtained with lower values of compaction load, pulse-on time and current and 30:70 (SiC:Cu) composition of tool. Analysis of variance is carried out and a significant COM model is observed with peak current yielding highest contribution followed by pulse-on time, compaction load and composition. The deposited layer is characterised by X-Ray Diffraction analysis which confirmed the presence of tool materials on the work piece surface.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3736458','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3736458"><span><span class="hlt">Design</span> and Experimental Evaluation of a <span class="hlt">Robust</span> Position Controller for an Electrohydrostatic Actuator Using Adaptive Antiwindup Sliding Mode Scheme</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lee, Ji Min; Park, Sung Hwan; Kim, Jong Shik</p> <p>2013-01-01</p> <p>A <span class="hlt">robust</span> control scheme is proposed for the position control of the electrohydrostatic actuator (EHA) when considering hardware saturation, load disturbance, and lumped system uncertainties and nonlinearities. To reduce overshoot due to a saturation of electric motor and to realize <span class="hlt">robustness</span> against load disturbance and lumped system uncertainties such as varying parameters and modeling error, this paper proposes an adaptive antiwindup PID sliding mode scheme as a <span class="hlt">robust</span> position controller for the EHA system. An optimal PID controller and an optimal anti-windup PID controller are also <span class="hlt">designed</span> to compare control performance. An EHA prototype is developed, carrying out system modeling and parameter identification in <span class="hlt">designing</span> the position controller. The simply identified linear model serves as the basis for the <span class="hlt">design</span> of the position controllers, while the <span class="hlt">robustness</span> of the control systems is compared by experiments. The adaptive anti-windup PID sliding mode controller has been found to have the desired performance and become <span class="hlt">robust</span> against hardware saturation, load disturbance, and lumped system uncertainties and nonlinearities. PMID:23983640</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25411131','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25411131"><span><span class="hlt">Design</span> of parallel transmission radiofrequency pulses <span class="hlt">robust</span> against respiration in cardiac MRI at 7 Tesla.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Schmitter, Sebastian; Wu, Xiaoping; Uğurbil, Kâmil; Van de Moortele, Pierre-François</p> <p>2015-11-01</p> <p>Two-spoke parallel transmission (pTX) radiofrequency (RF) pulses have been demonstrated in cardiac MRI at 7T. However, current pulse <span class="hlt">designs</span> rely on a single set of B1(+)/B0 maps that may not be valid for subsequent scans acquired at another phase of the respiration cycle because of organ displacement. Such mismatches may yield severe excitation profile degradation. B1(+)/B0 maps were obtained, using 16 transmit channels at 7T, at three breath-hold positions: exhale, half-inhale, and inhale. Standard and <span class="hlt">robust</span> RF pulses were <span class="hlt">designed</span> using maps obtained at exhale only, and at multiple respiratory positions, respectively. Excitation patterns were analyzed for all positions using Bloch simulations. Flip-angle homogeneity was compared in vivo in cardiac CINE acquisitions. Standard one- and two-spoke pTX RF pulses are sensitive to breath-hold position, primarily due to B1(+) alterations, with high dependency on excitation trajectory for two spokes. In vivo excitation inhomogeneity varied from nRMSE = 8.2% (exhale) up to 32.5% (inhale) with the standard <span class="hlt">design</span>; much more stable results were obtained with the <span class="hlt">robust</span> <span class="hlt">design</span> with nRMSE = 9.1% (exhale) and 10.6% (inhale). A new pTX RF pulse <span class="hlt">design</span> <span class="hlt">robust</span> against respiration induced variations of B1(+)/B0 maps is demonstrated and is expected to have a positive impact on cardiac MRI in breath-hold, free-breathing, and real-time acquisitions. © 2014 Wiley Periodicals, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16671630','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16671630"><span>Response to <span class="hlt">Taguchi</span> and Noma on "relationship between directionality and orientation in drawings by young children and adults.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Karev, George B</p> <p>2006-02-01</p> <p>When assessing the relationship between direction and orientation in drawings by young children and adults, <span class="hlt">Taguchi</span> and Noma used a fish-drawing task. However, the fish is not convenient enough as an object for such a task so it is highly preferable to use, instead of a single object, a set of several objects to assess directionality quantitatively. These authors' conclusions do not acknowledge alternative explanations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100036538','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100036538"><span><span class="hlt">Robust</span> Optimization <span class="hlt">Design</span> Algorithm for High-Frequency TWTs</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wilson, Jeffrey D.; Chevalier, Christine T.</p> <p>2010-01-01</p> <p>Traveling-wave tubes (TWTs), such as the Ka-band (26-GHz) model recently developed for the Lunar Reconnaissance Orbiter, are essential as communication amplifiers in spacecraft for virtually all near- and deep-space missions. This innovation is a computational <span class="hlt">design</span> algorithm that, for the first time, optimizes the efficiency and output power of a TWT while taking into account the effects of dimensional tolerance variations. Because they are primary power consumers and power generation is very expensive in space, much effort has been exerted over the last 30 years to increase the power efficiency of TWTs. However, at frequencies higher than about 60 GHz, efficiencies of TWTs are still quite low. A major reason is that at higher frequencies, dimensional tolerance variations from conventional micromachining techniques become relatively large with respect to the circuit dimensions. When this is the case, conventional <span class="hlt">design</span>- optimization procedures, which ignore dimensional variations, provide inaccurate <span class="hlt">designs</span> for which the actual amplifier performance substantially under-performs that of the <span class="hlt">design</span>. Thus, this new, <span class="hlt">robust</span> TWT optimization <span class="hlt">design</span> algorithm was created to take account of and ameliorate the deleterious effects of dimensional variations and to increase efficiency, power, and yield of high-frequency TWTs. This <span class="hlt">design</span> algorithm can help extend the use of TWTs into the terahertz frequency regime of 300-3000 GHz. Currently, these frequencies are under-utilized because of the lack of efficient amplifiers, thus this regime is known as the "terahertz gap." The development of an efficient terahertz TWT amplifier could enable breakthrough applications in space science molecular spectroscopy, remote sensing, nondestructive testing, high-resolution "through-the-wall" imaging, biomedical imaging, and detection of explosives and toxic biochemical agents.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMNH52A..08C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMNH52A..08C"><span>Assessing the <span class="hlt">Robustness</span> of Green Infrastructure under Stochastic <span class="hlt">Design</span> Storms and Climate Change Scenarios</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chui, T. F. M.; Yang, Y.</p> <p>2017-12-01</p> <p>Green infrastructures (GI) have been widely used to mitigate flood risk, improve surface water quality, and to restore predevelopment hydrologic regimes. Commonly-used GI include, bioretention system, porous pavement and green roof, etc. They are normally sized to fulfil different <span class="hlt">design</span> criteria (e.g. providing certain storage depths, limiting peak surface flow rates) that are formulated for current climate conditions. While GI commonly have long lifespan, the sensitivity of their performance to climate change is however unclear. This study first proposes a method to formulate suitable <span class="hlt">design</span> criteria to meet different management interests (e.g. different levels of first flush reduction and peak flow reduction). Then typical <span class="hlt">designs</span> of GI are proposed. In addition, a high resolution stochastic <span class="hlt">design</span> storm generator using copulas and random cascade model is developed, which is calibrated using recorded rainfall time series. Then, few climate change scenarios are generated by varying the duration and depth of <span class="hlt">design</span> storms, and changing the parameters of the calibrated storm generator. Finally, the performance of GI with typical <span class="hlt">designs</span> under the random synthesized <span class="hlt">design</span> storms are then assessed using numerical modeling. The <span class="hlt">robustness</span> of the <span class="hlt">designs</span> is obtained by the comparing their performance in the future scenarios to the current one. This study overall examines the <span class="hlt">robustness</span> of the current GI <span class="hlt">design</span> criteria under uncertain future climate conditions, demonstrating whether current GI <span class="hlt">design</span> criteria should be modified to account for climate change.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22630787','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22630787"><span>Hybrid surface <span class="hlt">design</span> for <span class="hlt">robust</span> superhydrophobicity.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dash, Susmita; Alt, Marie T; Garimella, Suresh V</p> <p>2012-06-26</p> <p>Surfaces may be rendered superhydrophobic by engineering the surface morphology to control the extent of the liquid-air interface and by the use of low-surface-energy coatings. The droplet state on a superhydrophobic surface under static and dynamic conditions may be explained in terms of the relative magnitudes of the wetting and antiwetting pressures acting at the liquid-air interface on the substrate. In this paper, we discuss the <span class="hlt">design</span> and fabrication of hollow hybrid superhydrophobic surfaces which incorporate both communicating and noncommunicating air gaps. The surface <span class="hlt">design</span> is analytically shown to exhibit higher capillary (or nonwetting) pressure compared to solid pillars with only communicating air gaps. Six hybrid surfaces are fabricated with different surface parameters selected such that the Cassie state of a droplet is energetically favorable. The <span class="hlt">robustness</span> of the surfaces is tested under dynamic impingement conditions, and droplet dynamics are explained using pressure-based transitions between Cassie and Wenzel states. During droplet impingement, the effective water hammer pressure acting due to the sudden change in the velocity of the droplet is determined experimentally and is found to be at least 2 orders of magnitude less than values reported in the literature. The experiments show that the water hammer pressure depends on the surface morphology and capillary pressure of the surface. We propose that the observed reduction in shock pressure may be attributed to the presence of air gaps in the substrate. This feature allows liquid deformation and hence avoids the sudden stoppage of the droplet motion as opposed to droplet behavior on smooth surfaces.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AcAau..71...92V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AcAau..71...92V"><span><span class="hlt">Design</span> of a <span class="hlt">robust</span> control law for the Vega launcher ballistic phase</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Valli, Monica; Lavagna, Michèle R.; Panozzo, Thomas</p> <p>2012-02-01</p> <p>This work presents the <span class="hlt">design</span> of a <span class="hlt">robust</span> control law, and the related control system architecture, for the Vega launcher ballistic phase, taking into account the complete six degrees of freedom dynamics. To gain <span class="hlt">robustness</span> a non-linear control approach has been preferred: more specifically the Lyapunov's second stability theorem has been exploited, being a very powerful tool to guarantee asymptotic stability of the controlled dynamics. The dynamics of Vega's actuators has also been taken into account. The system performance has been checked and analyzed by numerical simulations run on real mission data for different operational and configuration scenarios, and the effectiveness of the synthesized control highlighted: in particular scenarios including a wide range of composite's inertial configurations performing various typologies of maneuvers have been run. The <span class="hlt">robustness</span> of the controlled dynamics has been validated by 100 cases Monte Carlo analysis campaign: the containment of the dispersion for the controlled variables - say the composite roll, yaw and pitch angles - confirmed the wide validity and generality of the proposed control law. This paper will show the theoretical approach and discuss the obtained results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010JMagR.206..246C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010JMagR.206..246C"><span><span class="hlt">Robust</span> optimal <span class="hlt">design</span> of diffusion-weighted magnetic resonance experiments for skin microcirculation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Choi, J.; Raguin, L. G.</p> <p>2010-10-01</p> <p>Skin microcirculation plays an important role in several diseases including chronic venous insufficiency and diabetes. Magnetic resonance (MR) has the potential to provide quantitative information and a better penetration depth compared with other non-invasive methods such as laser Doppler flowmetry or optical coherence tomography. The continuous progress in hardware resulting in higher sensitivity must be coupled with advances in data acquisition schemes. In this article, we first introduce a physical model for quantifying skin microcirculation using diffusion-weighted MR (DWMR) based on an effective dispersion model for skin leading to a q-space model of the DWMR complex signal, and then <span class="hlt">design</span> the corresponding <span class="hlt">robust</span> optimal experiments. The resulting <span class="hlt">robust</span> optimal DWMR protocols improve the worst-case quality of parameter estimates using nonlinear least squares optimization by exploiting available a priori knowledge of model parameters. Hence, our approach optimizes the gradient strengths and directions used in DWMR experiments to <span class="hlt">robustly</span> minimize the size of the parameter estimation error with respect to model parameter uncertainty. Numerical evaluations are presented to demonstrate the effectiveness of our approach as compared to conventional DWMR protocols.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3589721','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3589721"><span>Laccase production by Coriolopsis caperata RCK2011: Optimization under solid state fermentation by <span class="hlt">Taguchi</span> DOE methodology</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Nandal, Preeti; Ravella, Sreenivas Rao; Kuhad, Ramesh Chander</p> <p>2013-01-01</p> <p>Laccase production by Coriolopsis caperata RCK2011 under solid state fermentation was optimized following <span class="hlt">Taguchi</span> <span class="hlt">design</span> of experiment. An orthogonal array layout of L18 (21 × 37) was constructed using Qualitek-4 software with eight most influensive factors on laccase production. At individual level pH contributed higher influence, whereas, corn steep liquor (CSL) accounted for more than 50% of the severity index with biotin and KH2PO4 at the interactive level. The optimum conditions derived were; temperature 30°C, pH 5.0, wheat bran 5.0 g, inoculum size 0.5 ml (fungal cell mass = 0.015 g dry wt.), biotin 0.5% w/v, KH2PO4 0.013% w/v, CSL 0.1% v/v and 0.5 mM xylidine as an inducer. The validation experiments using optimized conditions confirmed an improvement in enzyme production by 58.01%. The laccase production to the level of 1623.55 Ugds−1 indicates that the fungus C. caperata RCK2011 has the commercial potential for laccase. PMID:23463372</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900016053','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900016053"><span><span class="hlt">Robust</span> controller <span class="hlt">designs</span> for second-order dynamic system: A virtual passive approach</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Juang, Jer-Nan; Phan, Minh</p> <p>1990-01-01</p> <p>A <span class="hlt">robust</span> controller <span class="hlt">design</span> is presented for second-order dynamic systems. The controller is model-independent and itself is a virtual second-order dynamic system. Conditions on actuator and sensor placements are identified for controller <span class="hlt">designs</span> that guarantee overall closed-loop stability. The dynamic controller can be viewed as a virtual passive damping system that serves to stabilize the actual dynamic system. The control gains are interpreted as virtual mass, spring, and dashpot elements that play the same roles as actual physical elements in stability analysis. Position, velocity, and acceleration feedback are considered. Simple examples are provided to illustrate the physical meaning of this controller <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014EnOp...46..146N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014EnOp...46..146N"><span>Multi-objective <span class="hlt">robust</span> <span class="hlt">design</span> of energy-absorbing components using coupled process-performance simulations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Najafi, Ali; Acar, Erdem; Rais-Rohani, Masoud</p> <p>2014-02-01</p> <p>The stochastic uncertainties associated with the material, process and product are represented and propagated to process and performance responses. A finite element-based sequential coupled process-performance framework is used to simulate the forming and energy absorption responses of a thin-walled tube in a manner that both material properties and component geometry can evolve from one stage to the next for better prediction of the structural performance measures. Metamodelling techniques are used to develop surrogate models for manufacturing and performance responses. One set of metamodels relates the responses to the random variables whereas the other relates the mean and standard deviation of the responses to the selected <span class="hlt">design</span> variables. A multi-objective <span class="hlt">robust</span> <span class="hlt">design</span> optimization problem is formulated and solved to illustrate the methodology and the influence of uncertainties on manufacturability and energy absorption of a metallic double-hat tube. The results are compared with those of deterministic and augmented <span class="hlt">robust</span> optimization problems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008PhDT.......121T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008PhDT.......121T"><span>Aerodynamic <span class="hlt">design</span> applying automatic differentiation and using <span class="hlt">robust</span> variable fidelity optimization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Takemiya, Tetsushi</p> <p></p> <p>, and that (2) the AMF terminates optimization erroneously when the optimization problems have constraints. The first problem is due to inaccuracy in computing derivatives in the AMF, and the second problem is due to erroneous treatment of the trust region ratio, which sets the size of the domain for an optimization in the AMF. In order to solve the first problem of the AMF, automatic differentiation (AD) technique, which reads the codes of analysis models and automatically generates new derivative codes based on some mathematical rules, is applied. If derivatives are computed with the generated derivative code, they are analytical, and the required computational time is independent of the number of <span class="hlt">design</span> variables, which is very advantageous for realistic aerospace engineering problems. However, if analysis models implement iterative computations such as computational fluid dynamics (CFD), which solves system partial differential equations iteratively, computing derivatives through the AD requires a massive memory size. The author solved this deficiency by modifying the AD approach and developing a more efficient implementation with CFD, and successfully applied the AD to general CFD software. In order to solve the second problem of the AMF, the governing equation of the trust region ratio, which is very strict against the violation of constraints, is modified so that it can accept the violation of constraints within some tolerance. By accepting violations of constraints during the optimization process, the AMF can continue optimization without terminating immaturely and eventually find the true optimum <span class="hlt">design</span> point. With these modifications, the AMF is referred to as "<span class="hlt">Robust</span> AMF," and it is applied to airfoil and wing aerodynamic <span class="hlt">design</span> problems using Euler CFD software. The former problem has 21 <span class="hlt">design</span> variables, and the latter 64. In both problems, derivatives computed with the proposed AD method are first compared with those computed with the finite</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013EUCAS...6..749S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013EUCAS...6..749S"><span><span class="hlt">Robust</span> lateral blended-wing-body aircraft feedback control <span class="hlt">design</span> using a parameterized LFR model and DGK-iteration</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schirrer, A.; Westermayer, C.; Hemedi, M.; Kozek, M.</p> <p>2013-12-01</p> <p>This paper shows control <span class="hlt">design</span> results, performance, and limitations of <span class="hlt">robust</span> lateral control law <span class="hlt">designs</span> based on the DGK-iteration mixed-μ-synthesis procedure for a large, flexible blended wing body (BWB) passenger aircraft. The aircraft dynamics is preshaped by a low-complexity inner loop control law providing stabilization, basic response shaping, and flexible mode damping. The μ controllers are <span class="hlt">designed</span> to further improve vibration damping of the main flexible modes by exploiting the structure of the arising significant parameter-dependent plant variations. This is achieved by utilizing parameterized Linear Fractional Representations (LFR) of the aircraft rigid and flexible dynamics. <span class="hlt">Designs</span> with various levels of LFR complexity are carried out and discussed, showing the achieved performance improvement over the initial controller and their <span class="hlt">robustness</span> and complexity properties.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_13 --> <div id="page_14" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="261"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050220614','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050220614"><span>Advanced Vibration Analysis Tool Developed for <span class="hlt">Robust</span> Engine Rotor <span class="hlt">Designs</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Min, James B.</p> <p>2005-01-01</p> <p>The primary objective of this research program is to develop vibration analysis tools, <span class="hlt">design</span> tools, and <span class="hlt">design</span> strategies to significantly improve the safety and <span class="hlt">robustness</span> of turbine engine rotors. Bladed disks in turbine engines always feature small, random blade-to-blade differences, or mistuning. Mistuning can lead to a dramatic increase in blade forced-response amplitudes and stresses. Ultimately, this results in high-cycle fatigue, which is a major safety and cost concern. In this research program, the necessary steps will be taken to transform a state-of-the-art vibration analysis tool, the Turbo- Reduce forced-response prediction code, into an effective <span class="hlt">design</span> tool by enhancing and extending the underlying modeling and analysis methods. Furthermore, novel techniques will be developed to assess the safety of a given <span class="hlt">design</span>. In particular, a procedure will be established for using natural-frequency curve veerings to identify ranges of operating conditions (rotational speeds and engine orders) in which there is a great risk that the rotor blades will suffer high stresses. This work also will aid statistical studies of the forced response by reducing the necessary number of simulations. Finally, new strategies for improving the <span class="hlt">design</span> of rotors will be pursued.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JIEIC..98..541S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JIEIC..98..541S"><span>An Approach to Maximize Weld Penetration During TIG Welding of P91 Steel Plates by Utilizing Image Processing and <span class="hlt">Taguchi</span> Orthogonal Array</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Singh, Akhilesh Kumar; Debnath, Tapas; Dey, Vidyut; Rai, Ram Naresh</p> <p>2017-10-01</p> <p>P-91 is modified 9Cr-1Mo steel. Fabricated structures and components of P-91 has a lot of application in power and chemical industry owing to its excellent properties like high temperature stress corrosion resistance, less susceptibility to thermal fatigue at high operating temperatures. The weld quality and surface finish of fabricated structure of P91 is very good when welded by Tungsten Inert Gas welding (TIG). However, the process has its limitation regarding weld penetration. The success of a welding process lies in fabricating with such a combination of parameters that gives maximum weld penetration and minimum weld width. To carry out an investigation on the effect of the autogenous TIG welding parameters on weld penetration and weld width, bead-on-plate welds were carried on P91 plates of thickness 6 mm in accordance to a <span class="hlt">Taguchi</span> L9 <span class="hlt">design</span>. Welding current, welding speed and gas flow rate were the three control variables in the investigation. After autogenous (TIG) welding, the dimension of the weld width, weld penetration and weld area were successfully measured by an image analysis technique developed for the study. The maximum error for the measured dimensions of the weld width, penetration and area with the developed image analysis technique was only 2 % compared to the measurements of Leica-Q-Win-V3 software installed in optical microscope. The measurements with the developed software, unlike the measurements under a microscope, required least human intervention. An Analysis of Variance (ANOVA) confirms the significance of the selected parameters. Thereafter, <span class="hlt">Taguchi</span>'s method was successfully used to trade-off between maximum penetration and minimum weld width while keeping the weld area at a minimum.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19800010492','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19800010492"><span><span class="hlt">Robustness</span> results in LQG based multivariable control <span class="hlt">designs</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lehtomaki, N. A.; Sandell, N. R., Jr.; Athans, M.</p> <p>1980-01-01</p> <p>The <span class="hlt">robustness</span> of control systems with respect to model uncertainty is considered using simple frequency domain criteria. Results are derived under a common framework in which the minimum singular value of the return difference transfer matrix is the key quantity. In particular, the LQ and LQG <span class="hlt">robustness</span> results are discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016MS%26E..114a2033F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016MS%26E..114a2033F"><span>Experimental Validation for Hot Stamping Process by Using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fawzi Zamri, Mohd; Lim, Syh Kai; Razlan Yusoff, Ahmad</p> <p>2016-02-01</p> <p>Due to the demand for reduction in gas emissions, energy saving and producing safer vehicles has driven the development of Ultra High Strength Steel (UHSS) material. To strengthen UHSS material such as boron steel, it needed to undergo a process of hot stamping for heating at certain temperature and time. In this paper, <span class="hlt">Taguchi</span> method is applied to determine the appropriate parameter of thickness, heating temperature and heating time to achieve optimum strength of boron steel. The experiment is conducted by using flat square shape of hot stamping tool with tensile dog bone as a blank product. Then, the value of tensile strength and hardness is measured as response. The results showed that the lower thickness, higher heating temperature and heating time give the higher strength and hardness for the final product. In conclusion, boron steel blank are able to achieve up to 1200 MPa tensile strength and 650 HV of hardness.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29771666','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29771666"><span><span class="hlt">Robust</span> ADP <span class="hlt">Design</span> for Continuous-Time Nonlinear Systems With Output Constraints.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Fan, Bo; Yang, Qinmin; Tang, Xiaoyu; Sun, Youxian</p> <p>2018-06-01</p> <p>In this paper, a novel <span class="hlt">robust</span> adaptive dynamic programming (RADP)-based control strategy is presented for the optimal control of a class of output-constrained continuous-time unknown nonlinear systems. Our contribution includes a step forward beyond the usual optimal control result to show that the output of the plant is always within user-defined bounds. To achieve the new results, an error transformation technique is first established to generate an equivalent nonlinear system, whose asymptotic stability guarantees both the asymptotic stability and the satisfaction of the output restriction of the original system. Furthermore, RADP algorithms are developed to solve the transformed nonlinear optimal control problem with completely unknown dynamics as well as a <span class="hlt">robust</span> <span class="hlt">design</span> to guarantee the stability of the closed-loop systems in the presence of unavailable internal dynamic state. Via small-gain theorem, asymptotic stability of the original and transformed nonlinear system is theoretically guaranteed. Finally, comparison results demonstrate the merits of the proposed control policy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017NatSR...745297E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017NatSR...745297E"><span>Applying <span class="hlt">Taguchi</span> <span class="hlt">design</span> and large-scale strategy for mycosynthesis of nano-silver from endophytic Trichoderma harzianum SYA.F4 and its application against phytopathogens</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>El-Moslamy, Shahira H.; Elkady, Marwa F.; Rezk, Ahmed H.; Abdel-Fattah, Yasser R.</p> <p>2017-03-01</p> <p>Development of reliable and low-cost requirement for large-scale eco-friendly biogenic synthesis of metallic nanoparticles is an important step for industrial applications of bionanotechnology. In the present study, the mycosynthesis of spherical nano-Ag (12.7 ± 0.8 nm) from extracellular filtrate of local endophytic T. harzianum SYA.F4 strain which have interested mixed bioactive metabolites (alkaloids, flavonoids, tannins, phenols, nitrate reductase (320 nmol/hr/ml), carbohydrate (25 μg/μl) and total protein concentration (2.5 g/l) was reported. Industrial mycosynthesis of nano-Ag can be induced with different characters depending on the fungal cultivation and physical conditions. <span class="hlt">Taguchi</span> <span class="hlt">design</span> was applied to improve the physicochemical conditions for nano-Ag production, and the optimum conditions which increased its mass weight 3 times larger than a basal condition were as follows: AgNO3 (0.01 M), diluted reductant (10 v/v, pH 5) and incubated at 30 °C, 200 rpm for 24 hr. Kinetic conversion rates in submerged batch cultivation in 7 L stirred tank bioreactor on using semi-defined cultivation medium was as follows: the maximum biomass production (Xmax) and maximum nano-Ag mass weight (Pmax) calculated (60.5 g/l and 78.4 g/l respectively). The best nano-Ag concentration that formed large inhibition zones was 100 μg/ml which showed against A.alternate (43 mm) followed by Helminthosporium sp. (35 mm), Botrytis sp. (32 mm) and P. arenaria (28 mm).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1904b0006S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1904b0006S"><span>Application of <span class="hlt">Taguchi</span> optimization on the cassava starch wastewater electrocoagulation using batch recycle method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sudibyo, Hermida, L.; Suwardi</p> <p>2017-11-01</p> <p>Tapioca waste water is very difficult to treat; hence many tapioca factories could not treat it well. One of method which able to overcome this problem is electrodeposition. This process has high performance when it conducted using batch recycle process and use aluminum bipolar electrode. However, the optimum operation conditions are having a significant effect in the tapioca wastewater treatment using bath recycle process. In this research, The <span class="hlt">Taguchi</span> method was successfully applied to know the optimum condition and the interaction between parameters in electrocoagulation process. The results show that current density, conductivity, electrode distance, and pH have a significant effect on the turbidity removal of cassava starch waste water.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010PhyC..470.1986N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010PhyC..470.1986N"><span><span class="hlt">Robust</span> SMES controller <span class="hlt">design</span> for stabilization of inter-area oscillation considering coil size and system uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ngamroo, Issarachai</p> <p>2010-12-01</p> <p>It is well known that the superconducting magnetic energy storage (SMES) is able to quickly exchange active and reactive power with the power system. The SMES is expected to be the smart storage device for power system stabilization. Although the stabilizing effect of SMES is significant, the SMES is quite costly. Particularly, the superconducting magnetic coil size which is the essence of the SMES, must be carefully selected. On the other hand, various generation and load changes, unpredictable network structure, etc., cause system uncertainties. The power controller of SMES which is <span class="hlt">designed</span> without considering such uncertainties, may not tolerate and loses stabilizing effect. To overcome these problems, this paper proposes the new <span class="hlt">design</span> of <span class="hlt">robust</span> SMES controller taking coil size and system uncertainties into account. The structure of the active and reactive power controllers is the 1st-order lead-lag compensator. No need for the exact mathematical representation, system uncertainties are modeled by the inverse input multiplicative perturbation. Without the difficulty of the trade-off of damping performance and <span class="hlt">robustness</span>, the optimization problem of control parameters is formulated. The particle swarm optimization is used for solving the optimal parameters at each coil size automatically. Based on the normalized integral square error index and the consideration of coil current constraint, the <span class="hlt">robust</span> SMES with the smallest coil size which still provides the satisfactory stabilizing effect, can be achieved. Simulation studies in the two-area four-machine interconnected power system show the superior <span class="hlt">robustness</span> of the proposed <span class="hlt">robust</span> SMES with the smallest coil size under various operating conditions over the non-<span class="hlt">robust</span> SMES with large coil size.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17713623','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17713623"><span><span class="hlt">Design</span> and fabrication of chemically <span class="hlt">robust</span> three-dimensional microfluidic valves.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Maltezos, George; Garcia, Erika; Hanrahan, Grady; Gomez, Frank A; Vyawahare, Saurabh; Vyawhare, Saurabh; van Dam, R Michael; Chen, Yan; Scherer, Axel</p> <p>2007-09-01</p> <p>A current problem in microfluidics is that poly(dimethylsiloxane) (PDMS), used to fabricate many microfluidic devices, is not compatible with most organic solvents. Fluorinated compounds are more chemically <span class="hlt">robust</span> than PDMS but, historically, it has been nearly impossible to construct valves out of them by multilayer soft lithography (MSL) due to the difficulty of bonding layers made of "non-stick" fluoropolymers necessary to create traditional microfluidic valves. With our new three-dimensional (3D) valve <span class="hlt">design</span> we can fabricate microfluidic devices from fluorinated compounds in a single monolithic layer that is resistant to most organic solvents with minimal swelling. This paper describes the <span class="hlt">design</span> and development of 3D microfluidic valves by molding of a perfluoropolyether, termed Sifel, onto printed wax molds. The fabrication of Sifel-based microfluidic devices using this technique has great potential in chemical synthesis and analysis.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28416879','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28416879"><span>Supercritical CO2 extraction of candlenut oil: process optimization using <span class="hlt">Taguchi</span> orthogonal array and physicochemical properties of the oil.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Subroto, Erna; Widjojokusumo, Edward; Veriansyah, Bambang; Tjandrawinata, Raymond R</p> <p>2017-04-01</p> <p>A series of experiments was conducted to determine optimum conditions for supercritical carbon dioxide extraction of candlenut oil. A <span class="hlt">Taguchi</span> experimental <span class="hlt">design</span> with L 9 orthogonal array (four factors in three levels) was employed to evaluate the effects of pressure of 25-35 MPa, temperature of 40-60 °C, CO 2 flow rate of 10-20 g/min and particle size of 0.3-0.8 mm on oil solubility. The obtained results showed that increase in particle size, pressure and temperature improved the oil solubility. The supercritical carbon dioxide extraction at optimized parameters resulted in oil yield extraction of 61.4% at solubility of 9.6 g oil/kg CO 2 . The obtained candlenut oil from supercritical carbon dioxide extraction has better oil quality than oil which was extracted by Soxhlet extraction using n-hexane. The oil contains high unsaturated oil (linoleic acid and linolenic acid), which have many beneficial effects on human health.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19780040008&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19780040008&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda"><span><span class="hlt">Robustness</span> of linear quadratic state feedback <span class="hlt">designs</span> in the presence of system uncertainty. [application to Augmentor Wing Jet STOL Research Aircraft flare control autopilot <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Patel, R. V.; Toda, M.; Sridhar, B.</p> <p>1977-01-01</p> <p>The paper deals with the problem of expressing the <span class="hlt">robustness</span> (stability) property of a linear quadratic state feedback (LQSF) <span class="hlt">design</span> quantitatively in terms of bounds on the perturbations (modeling errors or parameter variations) in the system matrices so that the closed-loop system remains stable. Nonlinear time-varying and linear time-invariant perturbations are considered. The only computation required in obtaining a measure of the <span class="hlt">robustness</span> of an LQSF <span class="hlt">design</span> is to determine the eigenvalues of two symmetric matrices determined when solving the algebraic Riccati equation corresponding to the LQSF <span class="hlt">design</span> problem. Results are applied to a complex dynamic system consisting of the flare control of a STOL aircraft. The <span class="hlt">design</span> of the flare control is formulated as an LQSF tracking problem.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005PhDT........32F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005PhDT........32F"><span>Formulation of an integrated <span class="hlt">robust</span> <span class="hlt">design</span> and tactics optimization process for undersea weapon systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Frits, Andrew P.</p> <p></p> <p>In the current Navy environment of undersea weapons development, the engineering aspect of <span class="hlt">design</span> is decoupled from the development of the tactics with which the weapon is employed. Tactics are developed by intelligence experts, warfighters, and wargamers, while torpedo <span class="hlt">design</span> is handled by engineers and contractors. This dissertation examines methods by which the conceptual <span class="hlt">design</span> process of undersea weapon systems, including both torpedo systems and mine counter-measure systems, can be improved. It is shown that by simultaneously <span class="hlt">designing</span> the torpedo and the tactics with which undersea weapons are used, a more effective overall weapon system can be created. In addition to integrating torpedo tactics with <span class="hlt">design</span>, the thesis also looks at <span class="hlt">design</span> methods to account for uncertainty. The uncertainty is attributable to multiple sources, including: lack of detailed analysis tools early in the <span class="hlt">design</span> process, incomplete knowledge of the operational environments, and uncertainty in the performance of potential technologies. A <span class="hlt">robust</span> <span class="hlt">design</span> process is introduced to account for this uncertainty in the analysis and optimization of torpedo systems through the combination of Monte Carlo simulation with response surface methodology and metamodeling techniques. Additionally, various other methods that are appropriate to uncertainty analysis are discussed and analyzed. The thesis also advances a new approach towards examining <span class="hlt">robustness</span> and risk: the treatment of probability of success (POS) as an independent variable. Examining the cost and performance tradeoffs between high and low probability of success <span class="hlt">designs</span>, the decision-maker can make better informed decisions as to what <span class="hlt">designs</span> are most promising and determine the optimal balance of risk, cost, and performance. Finally, the thesis examines the use of non-dimensionalization of parameters for torpedo <span class="hlt">design</span>. The thesis shows that the use of non-dimensional torpedo parameters leads to increased knowledge about the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990095796','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990095796"><span>Critical Needs for <span class="hlt">Robust</span> and Reliable Database for <span class="hlt">Design</span> and Manufacturing of Ceramic Matrix Composites</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Singh, M.</p> <p>1999-01-01</p> <p>Ceramic matrix composite (CMC) components are being <span class="hlt">designed</span>, fabricated, and tested for a number of high temperature, high performance applications in aerospace and ground based systems. The critical need for and the role of reliable and <span class="hlt">robust</span> databases for the <span class="hlt">design</span> and manufacturing of ceramic matrix composites are presented. A number of issues related to engineering <span class="hlt">design</span>, manufacturing technologies, joining, and attachment technologies, are also discussed. Examples of various ongoing activities in the area of composite databases. <span class="hlt">designing</span> to codes and standards, and <span class="hlt">design</span> for manufacturing are given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012MSSP...32...44M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012MSSP...32...44M"><span>Reliability- and performance-based <span class="hlt">robust</span> <span class="hlt">design</span> optimization of MEMS structures considering technological uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Martowicz, Adam; Uhl, Tadeusz</p> <p>2012-10-01</p> <p>The paper discusses the applicability of a reliability- and performance-based multi-criteria <span class="hlt">robust</span> <span class="hlt">design</span> optimization technique for micro-electromechanical systems, considering their technological uncertainties. Nowadays, micro-devices are commonly applied systems, especially in the automotive industry, taking advantage of utilizing both the mechanical structure and electronic control circuit on one board. Their frequent use motivates the elaboration of virtual prototyping tools that can be applied in <span class="hlt">design</span> optimization with the introduction of technological uncertainties and reliability. The authors present a procedure for the optimization of micro-devices, which is based on the theory of reliability-based <span class="hlt">robust</span> <span class="hlt">design</span> optimization. This takes into consideration the performance of a micro-device and its reliability assessed by means of uncertainty analysis. The procedure assumes that, for each checked <span class="hlt">design</span> configuration, the assessment of uncertainty propagation is performed with the meta-modeling technique. The described procedure is illustrated with an example of the optimization carried out for a finite element model of a micro-mirror. The multi-physics approach allowed the introduction of several physical phenomena to correctly model the electrostatic actuation and the squeezing effect present between electrodes. The optimization was preceded by sensitivity analysis to establish the <span class="hlt">design</span> and uncertain domains. The genetic algorithms fulfilled the defined optimization task effectively. The best discovered individuals are characterized by a minimized value of the multi-criteria objective function, simultaneously satisfying the constraint on material strength. The restriction of the maximum equivalent stresses was introduced with the conditionally formulated objective function with a penalty component. The yielded results were successfully verified with a global uniform search through the input <span class="hlt">design</span> domain.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..1918888B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..1918888B"><span>Integrating operation <span class="hlt">design</span> into infrastructure planning to foster <span class="hlt">robustness</span> of planned water systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bertoni, Federica; Giuliani, Matteo; Castelletti, Andrea</p> <p>2017-04-01</p> <p>Over the past years, many studies have looked at the planning and management of water infrastructure systems as two separate problems, where the dynamic component (i.e., operations) is considered only after the static problem (i.e., planning) has been resolved. Most recent works have started to investigate planning and management as two strictly interconnected faces of the same problem, where the former is solved jointly with the latter in an integrated framework. This brings advantages to multi-purpose water reservoir systems, where several optimal operating strategies exist and similar system <span class="hlt">designs</span> might perform differently on the long term depending on the considered short-term operating tradeoff. An operationally <span class="hlt">robust</span> <span class="hlt">design</span> will be therefore one performing well across multiple feasible tradeoff operating policies. This work aims at studying the interaction between short-term operating strategies and their impacts on long-term structural decisions, when long-lived infrastructures with complex ecological impacts and multi-sectoral demands to satisfy (i.e., reservoirs) are considered. A parametric reinforcement learning approach is adopted for nesting optimization and control yielding to both optimal reservoir <span class="hlt">design</span> and optimal operational policies for water reservoir systems. The method is demonstrated on a synthetic reservoir that must be <span class="hlt">designed</span> and operated for ensuring reliable water supply to downstream users. At first, the optimal <span class="hlt">design</span> capacity derived is compared with the 'no-fail storage' computed through Rippl, a capacity <span class="hlt">design</span> function that returns the minimum storage needed to satisfy specified water demands without allowing supply shortfall. Then, the optimal reservoir volume is used to simulate the simplified case study under other operating objectives than water supply, in order to assess whether and how the system performance changes. The more <span class="hlt">robust</span> the infrastructural <span class="hlt">design</span>, the smaller the difference between the performances of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27259539','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27259539"><span><span class="hlt">Designing</span> <span class="hlt">robust</span> watermark barcodes for multiplex long-read sequencing.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ezpeleta, Joaquín; Krsticevic, Flavia J; Bulacio, Pilar; Tapia, Elizabeth</p> <p>2017-03-15</p> <p>To attain acceptable sample misassignment rates, current approaches to multiplex single-molecule real-time sequencing require upstream quality improvement, which is obtained from multiple passes over the sequenced insert and significantly reduces the effective read length. In order to fully exploit the raw read length on multiplex applications, <span class="hlt">robust</span> barcodes capable of dealing with the full single-pass error rates are needed. We present a method for <span class="hlt">designing</span> sequencing barcodes that can withstand a large number of insertion, deletion and substitution errors and are suitable for use in multiplex single-molecule real-time sequencing. The manuscript focuses on the <span class="hlt">design</span> of barcodes for full-length single-pass reads, impaired by challenging error rates in the order of 11%. The proposed barcodes can multiplex hundreds or thousands of samples while achieving sample misassignment probabilities as low as 10-7 under the above conditions, and are <span class="hlt">designed</span> to be compatible with chemical constraints imposed by the sequencing process. Software tools for constructing watermark barcode sets and demultiplexing barcoded reads, together with example sets of barcodes and synthetic barcoded reads, are freely available at www.cifasis-conicet.gov.ar/ezpeleta/NS-watermark . ezpeleta@cifasis-conicet.gov.ar. © The Author 2016. Published by Oxford University Press. All rights reserved. For Permissions, please e-mail: journals.permissions@oup.com</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22006659','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22006659"><span>Improving power and <span class="hlt">robustness</span> for detecting genetic association with extreme-value sampling <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Hua Yun; Li, Mingyao</p> <p>2011-12-01</p> <p>Extreme-value sampling <span class="hlt">design</span> that samples subjects with extremely large or small quantitative trait values is commonly used in genetic association studies. Samples in such <span class="hlt">designs</span> are often treated as "cases" and "controls" and analyzed using logistic regression. Such a case-control analysis ignores the potential dose-response relationship between the quantitative trait and the underlying trait locus and thus may lead to loss of power in detecting genetic association. An alternative approach to analyzing such data is to model the dose-response relationship by a linear regression model. However, parameter estimation from this model can be biased, which may lead to inflated type I errors. We propose a <span class="hlt">robust</span> and efficient approach that takes into consideration of both the biased sampling <span class="hlt">design</span> and the potential dose-response relationship. Extensive simulations demonstrate that the proposed method is more powerful than the traditional logistic regression analysis and is more <span class="hlt">robust</span> than the linear regression analysis. We applied our method to the analysis of a candidate gene association study on high-density lipoprotein cholesterol (HDL-C) which includes study subjects with extremely high or low HDL-C levels. Using our method, we identified several SNPs showing a stronger evidence of association with HDL-C than the traditional case-control logistic regression analysis. Our results suggest that it is important to appropriately model the quantitative traits and to adjust for the biased sampling when dose-response relationship exists in extreme-value sampling <span class="hlt">designs</span>. © 2011 Wiley Periodicals, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21994181','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21994181"><span><span class="hlt">Robust</span> tests for multivariate factorial <span class="hlt">designs</span> under heteroscedasticity.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Vallejo, Guillermo; Ato, Manuel</p> <p>2012-06-01</p> <p>The question of how to analyze several multivariate normal mean vectors when normality and covariance homogeneity assumptions are violated is considered in this article. For the two-way MANOVA layout, we address this problem adapting results presented by Brunner, Dette, and Munk (BDM; 1997) and Vallejo and Ato (modified Brown-Forsythe [MBF]; 2006) in the context of univariate factorial and split-plot <span class="hlt">designs</span> and a multivariate version of the linear model (MLM) to accommodate heterogeneous data. Furthermore, we compare these procedures with the Welch-James (WJ) approximate degrees of freedom multivariate statistics based on ordinary least squares via Monte Carlo simulation. Our numerical studies show that of the methods evaluated, only the modified versions of the BDM and MBF procedures were <span class="hlt">robust</span> to violations of underlying assumptions. The MLM approach was only occasionally liberal, and then by only a small amount, whereas the WJ procedure was often liberal if the interactive effects were involved in the <span class="hlt">design</span>, particularly when the number of dependent variables increased and total sample size was small. On the other hand, it was also found that the MLM procedure was uniformly more powerful than its most direct competitors. The overall success rate was 22.4% for the BDM, 36.3% for the MBF, and 45.0% for the MLM.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22105927-ap1000-sup-design-robustness-against-extreme-external-events-seismic-flooding-aircraft-crash','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22105927-ap1000-sup-design-robustness-against-extreme-external-events-seismic-flooding-aircraft-crash"><span>AP1000{sup R} <span class="hlt">design</span> <span class="hlt">robustness</span> against extreme external events - Seismic, flooding, and aircraft crash</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Pfister, A.; Goossen, C.; Coogler, K.</p> <p>2012-07-01</p> <p>Both the International Atomic Energy Agency (IAEA) and the U.S. Nuclear Regulatory Commission (NRC) require existing and new nuclear power plants to conduct plant assessments to demonstrate the unit's ability to withstand external hazards. The events that occurred at the Fukushima-Dai-ichi nuclear power station demonstrated the importance of <span class="hlt">designing</span> a nuclear power plant with the ability to protect the plant against extreme external hazards. The innovative <span class="hlt">design</span> of the AP1000{sup R} nuclear power plant provides unparalleled protection against catastrophic external events which can lead to extensive infrastructure damage and place the plant in an extended abnormal situation. The AP1000 plantmore » is an 1100-MWe pressurized water reactor with passive safety features and extensive plant simplifications that enhance construction, operation, maintenance and safety. The plant's compact safety related footprint and protection provided by its <span class="hlt">robust</span> nuclear island structures prevent significant damage to systems, structures, and components required to safely shutdown the plant and maintain core and spent fuel pool cooling and containment integrity following extreme external events. The AP1000 nuclear power plant has been extensively analyzed and reviewed to demonstrate that it's nuclear island <span class="hlt">design</span> and plant layout provide protection against both <span class="hlt">design</span> basis and extreme beyond <span class="hlt">design</span> basis external hazards such as extreme seismic events, external flooding that exceeds the maximum probable flood limit, and malicious aircraft impact. The AP1000 nuclear power plant uses fail safe passive features to mitigate <span class="hlt">design</span> basis accidents. The passive safety systems are <span class="hlt">designed</span> to function without safety-grade support systems (such as AC power, component cooling water, service water, compressed air or HVAC). The plant has been <span class="hlt">designed</span> to protect systems, structures, and components critical to placing the reactor in a safe shutdown condition within the steel containment</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596975','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596975"><span>A Unifying Mathematical Framework for Genetic <span class="hlt">Robustness</span>, Environmental <span class="hlt">Robustness</span>, Network <span class="hlt">Robustness</span> and their Trade-offs on Phenotype <span class="hlt">Robustness</span> in Biological Networks. Part III: Synthetic Gene Networks in Synthetic Biology</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chen, Bor-Sen; Lin, Ying-Po</p> <p>2013-01-01</p> <p><span class="hlt">Robust</span> stabilization and environmental disturbance attenuation are ubiquitous systematic properties that are observed in biological systems at many different levels. The underlying principles for <span class="hlt">robust</span> stabilization and environmental disturbance attenuation are universal to both complex biological systems and sophisticated engineering systems. In many biological networks, network <span class="hlt">robustness</span> should be large enough to confer: intrinsic <span class="hlt">robustness</span> for tolerating intrinsic parameter fluctuations; genetic <span class="hlt">robustness</span> for buffering genetic variations; and environmental <span class="hlt">robustness</span> for resisting environmental disturbances. Network <span class="hlt">robustness</span> is needed so phenotype stability of biological network can be maintained, guaranteeing phenotype <span class="hlt">robustness</span>. Synthetic biology is foreseen to have important applications in biotechnology and medicine; it is expected to contribute significantly to a better understanding of functioning of complex biological systems. This paper presents a unifying mathematical framework for investigating the principles of both <span class="hlt">robust</span> stabilization and environmental disturbance attenuation for synthetic gene networks in synthetic biology. Further, from the unifying mathematical framework, we found that the phenotype <span class="hlt">robustness</span> criterion for synthetic gene networks is the following: if intrinsic <span class="hlt">robustness</span> + genetic <span class="hlt">robustness</span> + environmental <span class="hlt">robustness</span> ≦ network <span class="hlt">robustness</span>, then the phenotype <span class="hlt">robustness</span> can be maintained in spite of intrinsic parameter fluctuations, genetic variations, and environmental disturbances. Therefore, the trade-offs between intrinsic <span class="hlt">robustness</span>, genetic <span class="hlt">robustness</span>, environmental <span class="hlt">robustness</span>, and network <span class="hlt">robustness</span> in synthetic biology can also be investigated through corresponding phenotype <span class="hlt">robustness</span> criteria from the systematic point of view. Finally, a <span class="hlt">robust</span> synthetic <span class="hlt">design</span> that involves network evolution algorithms with desired behavior under intrinsic parameter fluctuations, genetic variations, and environmental</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_14 --> <div id="page_15" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="281"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23515190','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23515190"><span>A Unifying Mathematical Framework for Genetic <span class="hlt">Robustness</span>, Environmental <span class="hlt">Robustness</span>, Network <span class="hlt">Robustness</span> and their Trade-offs on Phenotype <span class="hlt">Robustness</span> in Biological Networks. Part III: Synthetic Gene Networks in Synthetic Biology.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Bor-Sen; Lin, Ying-Po</p> <p>2013-01-01</p> <p><span class="hlt">Robust</span> stabilization and environmental disturbance attenuation are ubiquitous systematic properties that are observed in biological systems at many different levels. The underlying principles for <span class="hlt">robust</span> stabilization and environmental disturbance attenuation are universal to both complex biological systems and sophisticated engineering systems. In many biological networks, network <span class="hlt">robustness</span> should be large enough to confer: intrinsic <span class="hlt">robustness</span> for tolerating intrinsic parameter fluctuations; genetic <span class="hlt">robustness</span> for buffering genetic variations; and environmental <span class="hlt">robustness</span> for resisting environmental disturbances. Network <span class="hlt">robustness</span> is needed so phenotype stability of biological network can be maintained, guaranteeing phenotype <span class="hlt">robustness</span>. Synthetic biology is foreseen to have important applications in biotechnology and medicine; it is expected to contribute significantly to a better understanding of functioning of complex biological systems. This paper presents a unifying mathematical framework for investigating the principles of both <span class="hlt">robust</span> stabilization and environmental disturbance attenuation for synthetic gene networks in synthetic biology. Further, from the unifying mathematical framework, we found that the phenotype <span class="hlt">robustness</span> criterion for synthetic gene networks is the following: if intrinsic <span class="hlt">robustness</span> + genetic <span class="hlt">robustness</span> + environmental <span class="hlt">robustness</span> ≦ network <span class="hlt">robustness</span>, then the phenotype <span class="hlt">robustness</span> can be maintained in spite of intrinsic parameter fluctuations, genetic variations, and environmental disturbances. Therefore, the trade-offs between intrinsic <span class="hlt">robustness</span>, genetic <span class="hlt">robustness</span>, environmental <span class="hlt">robustness</span>, and network <span class="hlt">robustness</span> in synthetic biology can also be investigated through corresponding phenotype <span class="hlt">robustness</span> criteria from the systematic point of view. Finally, a <span class="hlt">robust</span> synthetic <span class="hlt">design</span> that involves network evolution algorithms with desired behavior under intrinsic parameter fluctuations, genetic variations, and environmental</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AIPC.1931c0029W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AIPC.1931c0029W"><span>Multi response optimization of internal grinding process parameters for outer ring using <span class="hlt">Taguchi</span> method and PCR-TOPSIS</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wisnuadi, Alief Regyan; Damayanti, Retno Wulan; Pujiyanto, Eko</p> <p>2018-02-01</p> <p>Bearing is one of the most widely used parts in automotive industry. One of the leading bearing manufacturing companies in the world is SKF Indonesia. This company must produce bearing with international standard. SKF Indonesia must do continuous improvement in order to face competition. During this time, SKF Indonesia is only performing quality control at its Quality Assurance department. In other words, quality improvement at SKF Indonesia has not been done thoroughly. The purpose of this research is to improve quality of outer ring product at SKF Indonesia by conducting an internal grinding process experiment about setting speed ratio, fine position, and spark out grinding time. The specific purpose of this experiment is to optimize some quality responses such as roughness, roundness, and cycle time. All of the response in this experiment were smaller the better. <span class="hlt">Taguchi</span> method and PCR-TOPSIS are used for the optimization process. The result of this research shows that by using <span class="hlt">Taguchi</span> method and PCR-TOPSIS, the optimum condition occurs on speed ratio 36, fine position 18 µm/s and spark out 0.5 s. The optimum conditions result were roughness 0.398 µm, roundness 1.78 µm and cycle time 8.1 s. This results have been better than the previous results and meet the standards. The roughness of 0.523 µm decrease to 0.398 µm and the average cycle time of 8.5 s decrease to 8.1 s.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18754384','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18754384"><span>Determining optimal operation parameters for reducing PCDD/F emissions (I-TEQ values) from the iron ore sintering process by using the <span class="hlt">Taguchi</span> experimental <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Yu-Cheng; Tsai, Perng-Jy; Mou, Jin-Luh</p> <p>2008-07-15</p> <p>This study is the first one using the <span class="hlt">Taguchi</span> experimental <span class="hlt">design</span> to identify the optimal operating condition for reducing polychlorinated dibenzo-p-dioxins and dibenzofurans (PCDD/ Fs) formations during the iron ore sintering process. Four operating parameters, including the water content (Wc; range = 6.0-7.0 wt %), suction pressure (Ps; range = 1000-1400 mmH2O), bed height (Hb; range = 500-600 mm), and type of hearth layer (including sinter, hematite, and limonite), were selected for conducting experiments in a pilot scale sinter pot to simulate various sintering operating conditions of a real-scale sinter plant We found that the resultant optimal combination (Wc = 6.5 wt%, Hb = 500 mm, Ps = 1000 mmH2O, and hearth layer = hematite) could decrease the emission factor of total PCDD/Fs (total EF(PCDD/Fs)) up to 62.8% by reference to the current operating condition of the real-scale sinter plant (Wc = 6.5 wt %, Hb = 550 mm, Ps = 1200 mmH2O, and hearth layer = sinter). Through the ANOVA analysis, we found that Wc was the most significant parameter in determining total EF(PCDD/Fs (accounting for 74.7% of the total contribution of the four selected parameters). The resultant optimal combination could also enhance slightly in both sinter productivity and sinter strength (30.3 t/m2/day and 72.4%, respectively) by reference to those obtained from the reference operating condition (29.9 t/m (2)/day and 72.2%, respectively). The above results further ensure the applicability of the obtained optimal combination for the real-scale sinter production without interfering its sinter productivity and sinter strength.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5368611','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5368611"><span>Applying <span class="hlt">Taguchi</span> <span class="hlt">design</span> and large-scale strategy for mycosynthesis of nano-silver from endophytic Trichoderma harzianum SYA.F4 and its application against phytopathogens</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>EL-Moslamy, Shahira H.; Elkady, Marwa F.; Rezk, Ahmed H.; Abdel-Fattah, Yasser R.</p> <p>2017-01-01</p> <p>Development of reliable and low-cost requirement for large-scale eco-friendly biogenic synthesis of metallic nanoparticles is an important step for industrial applications of bionanotechnology. In the present study, the mycosynthesis of spherical nano-Ag (12.7 ± 0.8 nm) from extracellular filtrate of local endophytic T. harzianum SYA.F4 strain which have interested mixed bioactive metabolites (alkaloids, flavonoids, tannins, phenols, nitrate reductase (320 nmol/hr/ml), carbohydrate (25 μg/μl) and total protein concentration (2.5 g/l) was reported. Industrial mycosynthesis of nano-Ag can be induced with different characters depending on the fungal cultivation and physical conditions. <span class="hlt">Taguchi</span> <span class="hlt">design</span> was applied to improve the physicochemical conditions for nano-Ag production, and the optimum conditions which increased its mass weight 3 times larger than a basal condition were as follows: AgNO3 (0.01 M), diluted reductant (10 v/v, pH 5) and incubated at 30 °C, 200 rpm for 24 hr. Kinetic conversion rates in submerged batch cultivation in 7 L stirred tank bioreactor on using semi-defined cultivation medium was as follows: the maximum biomass production (Xmax) and maximum nano-Ag mass weight (Pmax) calculated (60.5 g/l and 78.4 g/l respectively). The best nano-Ag concentration that formed large inhibition zones was 100 μg/ml which showed against A.alternate (43 mm) followed by Helminthosporium sp. (35 mm), Botrytis sp. (32 mm) and P. arenaria (28 mm). PMID:28349997</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25722723','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25722723"><span>Analytical quality by <span class="hlt">design</span>: a tool for regulatory flexibility and <span class="hlt">robust</span> analytics.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Peraman, Ramalingam; Bhadraya, Kalva; Padmanabha Reddy, Yiragamreddy</p> <p>2015-01-01</p> <p>Very recently, Food and Drug Administration (FDA) has approved a few new drug applications (NDA) with regulatory flexibility for quality by <span class="hlt">design</span> (QbD) based analytical approach. The concept of QbD applied to analytical method development is known now as AQbD (analytical quality by <span class="hlt">design</span>). It allows the analytical method for movement within method operable <span class="hlt">design</span> region (MODR). Unlike current methods, analytical method developed using analytical quality by <span class="hlt">design</span> (AQbD) approach reduces the number of out-of-trend (OOT) results and out-of-specification (OOS) results due to the <span class="hlt">robustness</span> of the method within the region. It is a current trend among pharmaceutical industry to implement analytical quality by <span class="hlt">design</span> (AQbD) in method development process as a part of risk management, pharmaceutical development, and pharmaceutical quality system (ICH Q10). Owing to the lack explanatory reviews, this paper has been communicated to discuss different views of analytical scientists about implementation of AQbD in pharmaceutical quality system and also to correlate with product quality by <span class="hlt">design</span> and pharmaceutical analytical technology (PAT).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4332986','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4332986"><span>Analytical Quality by <span class="hlt">Design</span>: A Tool for Regulatory Flexibility and <span class="hlt">Robust</span> Analytics</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Bhadraya, Kalva; Padmanabha Reddy, Yiragamreddy</p> <p>2015-01-01</p> <p>Very recently, Food and Drug Administration (FDA) has approved a few new drug applications (NDA) with regulatory flexibility for quality by <span class="hlt">design</span> (QbD) based analytical approach. The concept of QbD applied to analytical method development is known now as AQbD (analytical quality by <span class="hlt">design</span>). It allows the analytical method for movement within method operable <span class="hlt">design</span> region (MODR). Unlike current methods, analytical method developed using analytical quality by <span class="hlt">design</span> (AQbD) approach reduces the number of out-of-trend (OOT) results and out-of-specification (OOS) results due to the <span class="hlt">robustness</span> of the method within the region. It is a current trend among pharmaceutical industry to implement analytical quality by <span class="hlt">design</span> (AQbD) in method development process as a part of risk management, pharmaceutical development, and pharmaceutical quality system (ICH Q10). Owing to the lack explanatory reviews, this paper has been communicated to discuss different views of analytical scientists about implementation of AQbD in pharmaceutical quality system and also to correlate with product quality by <span class="hlt">design</span> and pharmaceutical analytical technology (PAT). PMID:25722723</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24327804','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24327804"><span>A <span class="hlt">robust</span> variable sampling time BLDC motor control <span class="hlt">design</span> based upon μ-synthesis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hung, Chung-Wen; Yen, Jia-Yush</p> <p>2013-01-01</p> <p>The variable sampling rate system is encountered in many applications. When the speed information is derived from the position marks along the trajectory, one would have a speed dependent sampling rate system. The conventional fixed or multisampling rate system theory may not work in these cases because the system dynamics include the uncertainties which resulted from the variable sampling rate. This paper derived a convenient expression for the speed dependent sampling rate system. The varying sampling rate effect is then translated into multiplicative uncertainties to the system. The <span class="hlt">design</span> then uses the popular μ-synthesis process to achieve a <span class="hlt">robust</span> performance controller <span class="hlt">design</span>. The implementation on a BLDC motor demonstrates the effectiveness of the <span class="hlt">design</span> approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3845655','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3845655"><span>A <span class="hlt">Robust</span> Variable Sampling Time BLDC Motor Control <span class="hlt">Design</span> Based upon μ-Synthesis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Yen, Jia-Yush</p> <p>2013-01-01</p> <p>The variable sampling rate system is encountered in many applications. When the speed information is derived from the position marks along the trajectory, one would have a speed dependent sampling rate system. The conventional fixed or multisampling rate system theory may not work in these cases because the system dynamics include the uncertainties which resulted from the variable sampling rate. This paper derived a convenient expression for the speed dependent sampling rate system. The varying sampling rate effect is then translated into multiplicative uncertainties to the system. The <span class="hlt">design</span> then uses the popular μ-synthesis process to achieve a <span class="hlt">robust</span> performance controller <span class="hlt">design</span>. The implementation on a BLDC motor demonstrates the effectiveness of the <span class="hlt">design</span> approach. PMID:24327804</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26030793','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26030793"><span>Bayes factors based on <span class="hlt">robust</span> TDT-type tests for family trio <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Yuan, Min; Pan, Xiaoqing; Yang, Yaning</p> <p>2015-06-01</p> <p>Adaptive transmission disequilibrium test (aTDT) and MAX3 test are two <span class="hlt">robust</span>-efficient association tests for case-parent family trio data. Both tests incorporate information of common genetic models including recessive, additive and dominant models and are efficient in power and <span class="hlt">robust</span> to genetic model specifications. The aTDT uses information of departure from Hardy-Weinberg disequilibrium to identify the potential genetic model underlying the data and then applies the corresponding TDT-type test, and the MAX3 test is defined as the maximum of the absolute value of three TDT-type tests under the three common genetic models. In this article, we propose three <span class="hlt">robust</span> Bayes procedures, the aTDT based Bayes factor, MAX3 based Bayes factor and Bayes model averaging (BMA), for association analysis with case-parent trio <span class="hlt">design</span>. The asymptotic distributions of aTDT under the null and alternative hypothesis are derived in order to calculate its Bayes factor. Extensive simulations show that the Bayes factors and the p-values of the corresponding tests are generally consistent and these Bayes factors are <span class="hlt">robust</span> to genetic model specifications, especially so when the priors on the genetic models are equal. When equal priors are used for the underlying genetic models, the Bayes factor method based on aTDT is more powerful than those based on MAX3 and Bayes model averaging. When the prior placed a small (large) probability on the true model, the Bayes factor based on aTDT (BMA) is more powerful. Analysis of a simulation data about RA from GAW15 is presented to illustrate applications of the proposed methods.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19780034150&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19780034150&hterms=toda&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dtoda"><span><span class="hlt">Robustness</span> in linear quadratic feedback <span class="hlt">design</span> with application to an aircraft control problem</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Patel, R. V.; Sridhar, B.; Toda, M.</p> <p>1977-01-01</p> <p>Some new results concerning <span class="hlt">robustness</span> and asymptotic properties of error bounds of a linear quadratic feedback <span class="hlt">design</span> are applied to an aircraft control problem. An autopilot for the flare control of the Augmentor Wing Jet STOL Research Aircraft (AWJSRA) is <span class="hlt">designed</span> based on Linear Quadratic (LQ) theory and the results developed in this paper. The variation of the error bounds to changes in the weighting matrices in the LQ <span class="hlt">design</span> is studied by computer simulations, and appropriate weighting matrices are chosen to obtain a reasonable error bound for variations in the system matrix and at the same time meet the practical constraints for the flare maneuver of the AWJSRA. Results from the computer simulation of a satisfactory autopilot <span class="hlt">design</span> for the flare control of the AWJSRA are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25352094','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25352094"><span>Mechanisms for <span class="hlt">Robust</span> Cognition.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Walsh, Matthew M; Gluck, Kevin A</p> <p>2015-08-01</p> <p>To function well in an unpredictable environment using unreliable components, a system must have a high degree of <span class="hlt">robustness</span>. <span class="hlt">Robustness</span> is fundamental to biological systems and is an objective in the <span class="hlt">design</span> of engineered systems such as airplane engines and buildings. Cognitive systems, like biological and engineered systems, exist within variable environments. This raises the question, how do cognitive systems achieve similarly high degrees of <span class="hlt">robustness</span>? The aim of this study was to identify a set of mechanisms that enhance <span class="hlt">robustness</span> in cognitive systems. We identify three mechanisms that enhance <span class="hlt">robustness</span> in biological and engineered systems: system control, redundancy, and adaptability. After surveying the psychological literature for evidence of these mechanisms, we provide simulations illustrating how each contributes to <span class="hlt">robust</span> cognition in a different psychological domain: psychomotor vigilance, semantic memory, and strategy selection. These simulations highlight features of a mathematical approach for quantifying <span class="hlt">robustness</span>, and they provide concrete examples of mechanisms for <span class="hlt">robust</span> cognition. © 2014 Cognitive Science Society, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950006369','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950006369"><span><span class="hlt">Robust</span> control <span class="hlt">design</span> with real parameter uncertainty using absolute stability theory. Ph.D. Thesis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>How, Jonathan P.; Hall, Steven R.</p> <p>1993-01-01</p> <p>The purpose of this thesis is to investigate an extension of mu theory for <span class="hlt">robust</span> control <span class="hlt">design</span> by considering systems with linear and nonlinear real parameter uncertainties. In the process, explicit connections are made between mixed mu and absolute stability theory. In particular, it is shown that the upper bounds for mixed mu are a generalization of results from absolute stability theory. Both state space and frequency domain criteria are developed for several nonlinearities and stability multipliers using the wealth of literature on absolute stability theory and the concepts of supply rates and storage functions. The state space conditions are expressed in terms of Riccati equations and parameter-dependent Lyapunov functions. For controller synthesis, these stability conditions are used to form an overbound of the H2 performance objective. A geometric interpretation of the equivalent frequency domain criteria in terms of off-axis circles clarifies the important role of the multiplier and shows that both the magnitude and phase of the uncertainty are considered. A numerical algorithm is developed to <span class="hlt">design</span> <span class="hlt">robust</span> controllers that minimize the bound on an H2 cost functional and satisfy an analysis test based on the Popov stability multiplier. The controller and multiplier coefficients are optimized simultaneously, which avoids the iteration and curve-fitting procedures required by the D-K procedure of mu synthesis. Several benchmark problems and experiments on the Middeck Active Control Experiment at M.I.T. demonstrate that these controllers achieve good <span class="hlt">robust</span> performance and guaranteed stability bounds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960029263','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960029263"><span>Application of Optimization Techniques to <span class="hlt">Design</span> of Unconventional Rocket Nozzle Configurations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Follett, W.; Ketchum, A.; Darian, A.; Hsu, Y.</p> <p>1996-01-01</p> <p>Several current rocket engine concepts such as the bell-annular tri-propellant engine, and the linear aerospike being proposed for the X-33 require unconventional three dimensional rocket nozzles which must conform to rectangular or sector shaped envelopes to meet integration constraints. These types of nozzles exist outside the current experience database, therefore, the application of efficient <span class="hlt">design</span> methods for these propulsion concepts is critical to the success of launch vehicle programs. The objective of this work is to optimize several different nozzle configurations, including two- and three-dimensional geometries. Methodology includes coupling computational fluid dynamic (CFD) analysis to genetic algorithms and <span class="hlt">Taguchi</span> methods as well as implementation of a streamline tracing technique. Results of applications are shown for several geometeries including: three dimensional thruster nozzles with round or super elliptic throats and rectangualar exits, two- and three-dimensional thrusters installed within a bell nozzle, and three dimensional thrusters with round throats and sector shaped exits. Due to the novel <span class="hlt">designs</span> considered for this study, there is little experience which can be used to guide the effort and limit the <span class="hlt">design</span> space. With a nearly infinite parameter space to explore, simple parametric <span class="hlt">design</span> studies cannot possibly search the entire <span class="hlt">design</span> space within the time frame required to impact the <span class="hlt">design</span> cycle. For this reason, <span class="hlt">robust</span> and efficient optimization methods are required to explore and exploit the <span class="hlt">design</span> space to achieve high performance engine <span class="hlt">designs</span>. Five case studies which examine the application of various techniques in the engineering environment are presented in this paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990025985','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990025985"><span>A Control Law <span class="hlt">Design</span> Method Facilitating Control Power, <span class="hlt">Robustness</span>, Agility, and Flying Qualities Tradeoffs: CRAFT</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Murphy, Patrick C.; Davidson, John B.</p> <p>1998-01-01</p> <p>A multi-input, multi-output control law <span class="hlt">design</span> methodology, named "CRAFT", is presented. CRAFT stands for the <span class="hlt">design</span> objectives addressed, namely, Control power, <span class="hlt">Robustness</span>, Agility, and Flying Qualities Tradeoffs. The methodology makes use of control law <span class="hlt">design</span> metrics from each of the four <span class="hlt">design</span> objective areas. It combines eigenspace assignment, which allows for direct specification of eigenvalues and eigenvectors, with a graphical approach for representing the metrics that captures numerous <span class="hlt">design</span> goals in one composite illustration. Sensitivity of the metrics to eigenspace choice is clearly displayed, enabling the <span class="hlt">designer</span> to assess the cost of <span class="hlt">design</span> tradeoffs. This approach enhances the <span class="hlt">designer</span>'s ability to make informed <span class="hlt">design</span> tradeoffs and to reach effective final <span class="hlt">designs</span>. An example of the CRAFT methodology applied to an advanced experimental fighter and discussion of associated <span class="hlt">design</span> issues are provided.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123c5701C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123c5701C"><span>Electronic structure <span class="hlt">robustness</span> and <span class="hlt">design</span> rules for 2D colloidal heterostructures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chu, Audrey; Livache, Clément; Ithurria, Sandrine; Lhuillier, Emmanuel</p> <p>2018-01-01</p> <p>Among the colloidal quantum dots, 2D nanoplatelets present exceptionally narrow optical features. Rationalizing the <span class="hlt">design</span> of heterostructures of these objects is of utmost interest; however, very little work has been focused on the investigation of their electronic properties. This work is organized into two main parts. In the first part, we use 1D solving of the Schrödinger equation to extract the effective masses for nanoplatelets (NPLs) of CdSe, CdS, and CdTe and the valence band offset for NPL core/shell of CdSe/CdS. In the second part, using the determined parameters, we quantize how the spectra of the CdSe/CdS heterostructure get affected by (i) the application of an electric field and (ii) by the presence of a dull interface. We also propose <span class="hlt">design</span> strategies to make the heterostructure even more <span class="hlt">robust</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1017985','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1017985"><span>Non-Linear Metamodeling Extensions to the <span class="hlt">Robust</span> Parameter <span class="hlt">Design</span> of Computer Simulations</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2016-09-15</p> <p><span class="hlt">design</span> By principal component analysis," Total Quality Management, vol. 8, no. 6, pp. 409-416, 1997. [25] A. Salmasnia, R. B . Kazemzadeh and S. T . A...and D. T . Sturrock, Simulation with Arena (3rd ed.), New York, NY: McGraw-Hill, 2004. [85] A. M. Mathai and S. B . Provost, Quadratic Forms in Random...PhD Member ADEDEJI B . BADIRU, PhD Dean, Graduate School of Engineering and Management iv AFIT-ENS-DS-16-S-026 Abstract <span class="hlt">Robust</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..184a2018M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..184a2018M"><span>Abrasive wear response of TIG-melted TiC composite coating: <span class="hlt">Taguchi</span> approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Maleque, M. A.; Bello, K. A.; Adebisi, A. A.; Dube, A.</p> <p>2017-03-01</p> <p>In this study, <span class="hlt">Taguchi</span> <span class="hlt">design</span> of experiment approach has been applied to assess wear behaviour of TiC composite coatings deposited on AISI 4340 steel substrates by novel powder preplacement and TIG torch melting processes. To study the abrasive wear behaviour of these coatings against alumina ball at 600° C, a Taguchi’s orthogonal array is used to acquire the wear test data for determining optimal parameters that lead to the minimization of wear rate. Composite coatings are developed based on Taguchi’s L-16 orthogonal array experiment with three process parameters (welding current, welding speed, welding voltage and shielding gas flow rate) at four levels. In this technique, mean response and signal-to-noise ratio are used to evaluate the influence of the TIG process parameters on the wear rate performance of the composite coated surfaces. The results reveal that welding voltage is the most significant control parameter for minimizing wear rate while the current presents the least contribution to the wear rate reduction. The study also shows the best optimal condition has been arrived at A3 (90 A), B4 (2.5 mm/s), C3 (30 V) and D3 (20 L/min), which gives minimum wear rate in TiC embedded coatings. Finally, a confirmatory experiment has been conducted to verify the optimized result and shows that the error between the predicted values and the experimental observation at the optimal condition lies within the limit of 4.7 %. Thus, the validity of the optimum condition for the coatings is established.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015OptLE..67...94R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015OptLE..67...94R"><span>Parameters optimization of laser brazing in crimping butt using <span class="hlt">Taguchi</span> and BPNN-GA</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rong, Youmin; Zhang, Zhen; Zhang, Guojun; Yue, Chen; Gu, Yafei; Huang, Yu; Wang, Chunming; Shao, Xinyu</p> <p>2015-04-01</p> <p>The laser brazing (LB) is widely used in the automotive industry due to the advantages of high speed, small heat affected zone, high quality of welding seam, and low heat input. Welding parameters play a significant role in determining the bead geometry and hence quality of the weld joint. This paper addresses the optimization of the seam shape in LB process with welding crimping butt of 0.8 mm thickness using back propagation neural network (BPNN) and genetic algorithm (GA). A 3-factor, 5-level welding experiment is conducted by <span class="hlt">Taguchi</span> L25 orthogonal array through the statistical <span class="hlt">design</span> method. Then, the input parameters are considered here including welding speed, wire speed rate, and gap with 5 levels. The output results are efficient connection length of left side and right side, top width (WT) and bottom width (WB) of the weld bead. The experiment results are embed into the BPNN network to establish relationship between the input and output variables. The predicted results of the BPNN are fed to GA algorithm that optimizes the process parameters subjected to the objectives. Then, the effects of welding speed (WS), wire feed rate (WF), and gap (GAP) on the sum values of bead geometry is discussed. Eventually, the confirmation experiments are carried out to demonstrate the optimal values were effective and reliable. On the whole, the proposed hybrid method, BPNN-GA, can be used to guide the actual work and improve the efficiency and stability of LB process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://pubs.er.usgs.gov/publication/5211457','USGSPUBS'); return false;" href="https://pubs.er.usgs.gov/publication/5211457"><span>A traditional and a less-invasive <span class="hlt">robust</span> <span class="hlt">design</span>: choices in optimizing effort allocation for seabird population studies</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Converse, S.J.; Kendall, W.L.; Doherty, P.F.; Naughton, M.B.; Hines, J.E.; Thomson, David L.; Cooch, Evan G.; Conroy, Michael J.</p> <p>2009-01-01</p> <p>For many animal populations, one or more life stages are not accessible to sampling, and therefore an unobservable state is created. For colonially-breeding populations, this unobservable state could represent the subset of adult breeders that have foregone breeding in a given year. This situation applies to many seabird populations, notably albatrosses, where skipped breeders are either absent from the colony, or are present but difficult to capture or correctly assign to breeding state. Kendall et al. have proposed <span class="hlt">design</span> strategies for investigations of seabird demography where such temporary emigration occurs, suggesting the use of the <span class="hlt">robust</span> <span class="hlt">design</span> to permit the estimation of time-dependent parameters and to increase the precision of estimates from multi-state models. A traditional <span class="hlt">robust</span> <span class="hlt">design</span>, where animals are subject to capture multiple times in a sampling season, is feasible in many cases. However, due to concerns that multiple captures per season could cause undue disturbance to animals, Kendall et al. developed a less-invasive <span class="hlt">robust</span> <span class="hlt">design</span> (LIRD), where initial captures are followed by an assessment of the ratio of marked-to-unmarked birds in the population or sampled plot. This approach has recently been applied in the Northwestern Hawaiian Islands to populations of Laysan (Phoebastria immutabilis) and black-footed (P. nigripes) albatrosses. In this paper, we outline the LIRD and its application to seabird population studies. We then describe an approach to determining optimal allocation of sampling effort in which we consider a non-<span class="hlt">robust</span> <span class="hlt">design</span> option (nRD), and variations of both the traditional <span class="hlt">robust</span> <span class="hlt">design</span> (RD), and the LIRD. Variations we considered included the number of secondary sampling occasions for the RD and the amount of total effort allocated to the marked-to-unmarked ratio assessment for the LIRD. We used simulations, informed by early data from the Hawaiian study, to address optimal study <span class="hlt">design</span> for our example cases. We found that</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26347006','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26347006"><span>Modular <span class="hlt">design</span> of metabolic network for <span class="hlt">robust</span> production of n-butanol from galactose-glucose mixtures.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lim, Hyun Gyu; Lim, Jae Hyung; Jung, Gyoo Yeol</p> <p>2015-01-01</p> <p>Refactoring microorganisms for efficient production of advanced biofuel such as n-butanol from a mixture of sugars in the cheap feedstock is a prerequisite to achieve economic feasibility in biorefinery. However, production of biofuel from inedible and cheap feedstock is highly challenging due to the slower utilization of biomass-driven sugars, arising from complex assimilation pathway, difficulties in amplification of biosynthetic pathways for heterologous metabolite, and redox imbalance caused by consuming intracellular reducing power to produce quite reduced biofuel. Even with these problems, the microorganisms should show <span class="hlt">robust</span> production of biofuel to obtain industrial feasibility. Thus, refactoring microorganisms for efficient conversion is highly desirable in biofuel production. In this study, we engineered <span class="hlt">robust</span> Escherichia coli to accomplish high production of n-butanol from galactose-glucose mixtures via the <span class="hlt">design</span> of modular pathway, an efficient and systematic way, to reconstruct the entire metabolic pathway with many target genes. Three modular pathways <span class="hlt">designed</span> using the predictable genetic elements were assembled for efficient galactose utilization, n-butanol production, and redox re-balancing to <span class="hlt">robustly</span> produce n-butanol from a sugar mixture of galactose and glucose. Specifically, the engineered strain showed dramatically increased n-butanol production (3.3-fold increased to 6.2 g/L after 48-h fermentation) compared to the parental strain (1.9 g/L) in galactose-supplemented medium. Moreover, fermentation with mixtures of galactose and glucose at various ratios from 2:1 to 1:2 confirmed that our engineered strain was able to <span class="hlt">robustly</span> produce n-butanol regardless of sugar composition with simultaneous utilization of galactose and glucose. Collectively, modular pathway engineering of metabolic network can be an effective approach in strain development for optimal biofuel production with cost-effective fermentable sugars. To the best of our</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_15 --> <div id="page_16" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="301"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008PhRvE..77c1922H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008PhRvE..77c1922H"><span>Least dissipation cost as a <span class="hlt">design</span> principle for <span class="hlt">robustness</span> and function of cellular networks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Han, Bo; Wang, Jin</p> <p>2008-03-01</p> <p>From a study of the budding yeast cell cycle, we found that the cellular network evolves to have the least cost for realizing its biological function. We quantify the cost in terms of the dissipation or heat loss characterized through the steady-state properties: the underlying landscape and the associated flux. We found that the dissipation cost is intimately related to the stability and <span class="hlt">robustness</span> of the network. With the least dissipation cost, the network becomes most stable and <span class="hlt">robust</span> under mutations and perturbations on the sharpness of the response from input to output as well as self-degradations. The least dissipation cost may provide a general <span class="hlt">design</span> principle for the cellular network to survive from the evolution and realize the biological function.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EJASP2017...55M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EJASP2017...55M"><span><span class="hlt">Robust</span> transceiver <span class="hlt">design</span> for reciprocal M × N interference channel based on statistical linearization approximation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mayvan, Ali D.; Aghaeinia, Hassan; Kazemi, Mohammad</p> <p>2017-12-01</p> <p>This paper focuses on <span class="hlt">robust</span> transceiver <span class="hlt">design</span> for throughput enhancement on the interference channel (IC), under imperfect channel state information (CSI). In this paper, two algorithms are proposed to improve the throughput of the multi-input multi-output (MIMO) IC. Each transmitter and receiver has, respectively, M and N antennas and IC operates in a time division duplex mode. In the first proposed algorithm, each transceiver adjusts its filter to maximize the expected value of signal-to-interference-plus-noise ratio (SINR). On the other hand, the second algorithm tries to minimize the variances of the SINRs to hedge against the variability due to CSI error. Taylor expansion is exploited to approximate the effect of CSI imperfection on mean and variance. The proposed <span class="hlt">robust</span> algorithms utilize the reciprocity of wireless networks to optimize the estimated statistical properties in two different working modes. Monte Carlo simulations are employed to investigate sum rate performance of the proposed algorithms and the advantage of incorporating variation minimization into the transceiver <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=biologicals&pg=3&id=EJ1069847','ERIC'); return false;" href="https://eric.ed.gov/?q=biologicals&pg=3&id=EJ1069847"><span>Mechanisms for <span class="hlt">Robust</span> Cognition</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Walsh, Matthew M.; Gluck, Kevin A.</p> <p>2015-01-01</p> <p>To function well in an unpredictable environment using unreliable components, a system must have a high degree of <span class="hlt">robustness</span>. <span class="hlt">Robustness</span> is fundamental to biological systems and is an objective in the <span class="hlt">design</span> of engineered systems such as airplane engines and buildings. Cognitive systems, like biological and engineered systems, exist within…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26584152','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26584152"><span>Optimization of delignification of two Pennisetum grass species by NaOH pretreatment using <span class="hlt">Taguchi</span> and ANN statistical approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mohaptra, Sonali; Dash, Preeti Krishna; Behera, Sudhanshu Shekar; Thatoi, Hrudayanath</p> <p>2016-01-01</p> <p>In the bioconversion of lignocelluloses for bioethanol, pretreatment seems to be the most important step which improves the elimination of the lignin and hemicelluloses content, exposing cellulose to further hydrolysis. The present study discusses the application of dynamic statistical techniques like the <span class="hlt">Taguchi</span> method and artificial neural network (ANN) in the optimization of pretreatment of lignocellulosic biomasses such as Hybrid Napier grass (HNG) (Pennisetum purpureum) and Denanath grass (DG) (Pennisetum pedicellatum), using alkali sodium hydroxide. This study analysed and determined a parameter combination with a low number of experiments by using the <span class="hlt">Taguchi</span> method in which both the substrates can be efficiently pretreated. The optimized parameters obtained from the L16 orthogonal array are soaking time (18 and 26 h), temperature (60°C and 55°C), and alkali concentration (1%) for HNG and DG, respectively. High performance liquid chromatography analysis of the optimized pretreated grass varieties confirmed the presence of glucan (47.94% and 46.50%), xylan (9.35% and 7.95%), arabinan (2.15% and 2.2%), and galactan/mannan (1.44% and 1.52%) for HNG and DG, respectively. Physicochemical characterization studies of native and alkali-pretreated grasses were carried out by scanning electron microscopy and Fourier transformation Infrared spectroscopy which revealed some morphological differences between the native and optimized pretreated samples. Model validation by ANN showed a good agreement between experimental results and the predicted responses.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28431349','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28431349"><span>Impacts of environmental factors on arsenate biotransformation and release in Microcystis aeruginosa using the <span class="hlt">Taguchi</span> experimental <span class="hlt">design</span> approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wang, Zhenhong; Luo, Zhuanxi; Yan, Changzhou; Xing, Baoshan</p> <p>2017-07-01</p> <p>Very limited information is available on how and to what extent environmental factors influence arsenic (As) biotransformation and release in freshwater algae. These factors include concentrations of arsenate (As(V)), dissolved inorganic nitrogen (N), phosphate (P), and ambient pH. This study conducted a series of experiments using <span class="hlt">Taguchi</span> methods to determine optimum conditions for As biotransformation. We assessed principal effective factors of As(V), N, P, and pH and determined that As biotransformation and release actuate at 10.0 μM As(V) in dead alga cells, the As efflux ratio and organic As efflux content actuate at 1.0 mg/L P, algal growth and intracellular arsenite (As(III)) content actuate at 10.0 mg/L N, and the total sum of As(III) efflux from dead alga cells actuates at a pH level of 10. Moreover, N is the critical component for As(V) biotransformation in M. aeruginosa, specifically for As(III) transformation, because N can accelerate algal growth, subsequently improving As(III) accumulation and its efflux, which results in an As(V) to As(III) reduction. Furthermore, low P concentrations in combination with high N concentrations promote As accumulation. Following As(V), P was the primary impacting factor for As accumulation. In addition, small amounts of As accumulation under low concentrations of As and high P were securely stored in living algal cells and were easily released after cell death. Results from this study will help to assess practical applications and the overall control of key environmental factors, particularly those associated with algal bioremediation in As polluted water. Copyright © 2017 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26167525','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26167525"><span>Free-Energy-Based <span class="hlt">Design</span> Policy for <span class="hlt">Robust</span> Network Control against Environmental Fluctuation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Iwai, Takuya; Kominami, Daichi; Murata, Masayuki; Yomo, Tetsuya</p> <p>2015-01-01</p> <p>Bioinspired network control is a promising approach for realizing <span class="hlt">robust</span> network controls. It relies on a probabilistic mechanism composed of positive and negative feedback that allows the system to eventually stabilize on the best solution. When the best solution fails due to environmental fluctuation, the system cannot keep its function until the system finds another solution again. To prevent the temporal loss of the function, the system should prepare some solution candidates and stochastically select available one from them. However, most bioinspired network controls are not <span class="hlt">designed</span> with this issue in mind. In this paper, we propose a thermodynamics-based <span class="hlt">design</span> policy that allows systems to retain an appropriate degree of randomness depending on the degree of environmental fluctuation, which prepares the system for the occurrence of environmental fluctuation. Furthermore, we verify the <span class="hlt">design</span> policy by using an attractor selection model-based multipath routing to run simulation experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18572188','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18572188"><span>Optimizing ELISAs for precision and <span class="hlt">robustness</span> using laboratory automation and statistical <span class="hlt">design</span> of experiments.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Joelsson, Daniel; Moravec, Phil; Troutman, Matthew; Pigeon, Joseph; DePhillips, Pete</p> <p>2008-08-20</p> <p>Transferring manual ELISAs to automated platforms requires optimizing the assays for each particular robotic platform. These optimization experiments are often time consuming and difficult to perform using a traditional one-factor-at-a-time strategy. In this manuscript we describe the development of an automated process using statistical <span class="hlt">design</span> of experiments (DOE) to quickly optimize immunoassays for precision and <span class="hlt">robustness</span> on the Tecan EVO liquid handler. By using fractional factorials and a split-plot <span class="hlt">design</span>, five incubation time variables and four reagent concentration variables can be optimized in a short period of time.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..225a2165V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..225a2165V"><span>Comparative Assessment of Cutting Inserts and Optimization during Hard Turning: <span class="hlt">Taguchi</span>-Based Grey Relational Analysis</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Venkata Subbaiah, K.; Raju, Ch.; Suresh, Ch.</p> <p>2017-08-01</p> <p>The present study aims to compare the conventional cutting inserts with wiper cutting inserts during the hard turning of AISI 4340 steel at different workpiece hardness. Type of insert, hardness, cutting speed, feed, and depth of cut are taken as process parameters. Taguchi’s L18 orthogonal array was used to conduct the experimental tests. Parametric analysis carried in order to know the influence of each process parameter on the three important Surface Roughness Characteristics (Ra, Rz, and Rt) and Material Removal Rate. <span class="hlt">Taguchi</span> based Grey Relational Analysis (GRA) used to optimize the process parameters for individual response and multi-response outputs. Additionally, the analysis of variance (ANOVA) is also applied to identify the most significant factor.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900017046','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900017046"><span>Intergration of system identification and <span class="hlt">robust</span> controller <span class="hlt">designs</span> for flexible structures in space</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Juang, Jer-Nan; Lew, Jiann-Shiun</p> <p>1990-01-01</p> <p>An approach is developed using experimental data to identify a reduced-order model and its model error for a <span class="hlt">robust</span> controller <span class="hlt">design</span>. There are three steps involved in the approach. First, an approximately balanced model is identified using the Eigensystem Realization Algorithm, which is an identification algorithm. Second, the model error is calculated and described in frequency domain in terms of the H(infinity) norm. Third, a pole placement technique in combination with a H(infinity) control method is applied to <span class="hlt">design</span> a controller for the considered system. A set experimental data from an existing setup, namely the Mini-Mast system, is used to illustrate and verify the approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017IJMPB..3144046P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017IJMPB..3144046P"><span>Parameter optimization of flux-aided backing-submerged arc welding by using <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pu, Juan; Yu, Shengfu; Li, Yuanyuan</p> <p>2017-07-01</p> <p>Flux-aided backing-submerged arc welding has been conducted on D36 steel with thickness of 20 mm. The effects of processing parameters such as welding current, voltage, welding speed and groove angle on welding quality were investigated by <span class="hlt">Taguchi</span> method. The optimal welding parameters were predicted and the individual importance of each parameter on welding quality was evaluated by examining the signal-to-noise ratio and analysis of variance (ANOVA) results. The importance order of the welding parameters for the welding quality of weld bead was: welding current > welding speed > groove angle > welding voltage. The welding quality of weld bead increased gradually with increasing welding current and welding speed and decreasing groove angle. The optimum values of the welding current, welding speed, groove angle and welding voltage were found to be 1050 A, 27 cm/min, 40∘ and 34 V, respectively.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040129587','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040129587"><span>Elements of <span class="hlt">Designing</span> for Cost</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dean, Edwin B.; Unal, Resit</p> <p>1992-01-01</p> <p>During recent history in the United States, government systems development has been performance driven. As a result, systems within a class have experienced exponentially increasing cost over time in fixed year dollars. Moreover, little emphasis has been placed on reducing cost. This paper defines <span class="hlt">designing</span> for cost and presents several tools which, if used in the engineering process, offer the promise of reducing cost. Although other potential tools exist for <span class="hlt">designing</span> for cost, this paper focuses on rules of thumb, quality function deployment, <span class="hlt">Taguchi</span> methods, concurrent engineering, and activity based costing. Each of these tools has been demonstrated to reduce cost if used within the engineering process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920050611&hterms=1057&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3D%2526%25231057','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920050611&hterms=1057&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3D%2526%25231057"><span>Elements of <span class="hlt">designing</span> for cost</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dean, Edwin B.; Unal, Resit</p> <p>1992-01-01</p> <p>During recent history in the United States, government systems development has been performance driven. As a result, systems within a class have experienced exponentially increasing cost over time in fixed year dollars. Moreover, little emphasis has been placed on reducing cost. This paper defines <span class="hlt">designing</span> for cost and presents several tools which, if used in the engineering process, offer the promise of reducing cost. Although other potential tools exist for <span class="hlt">designing</span> for cost, this paper focuses on rules of thumb, quality function deployment, <span class="hlt">Taguchi</span> methods, concurrent engineering, and activity-based costing. Each of these tools has been demonstrated to reduce cost if used within the engineering process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960052915','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960052915"><span><span class="hlt">Design</span> of <span class="hlt">Robust</span> Adaptive Unbalance Response Controllers for Rotors with Magnetic Bearings</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Knospe, Carl R.; Tamer, Samir M.; Fedigan, Stephen J.</p> <p>1996-01-01</p> <p>Experimental results have recently demonstrated that an adaptive open loop control strategy can be highly effective in the suppression of unbalance induced vibration on rotors supported in active magnetic bearings. This algorithm, however, relies upon a predetermined gain matrix. Typically, this matrix is determined by an optimal control formulation resulting in the choice of the pseudo-inverse of the nominal influence coefficient matrix as the gain matrix. This solution may result in problems with stability and performance <span class="hlt">robustness</span> since the estimated influence coefficient matrix is not equal to the actual influence coefficient matrix. Recently, analysis tools have been developed to examine the <span class="hlt">robustness</span> of this control algorithm with respect to structured uncertainty. Herein, these tools are extended to produce a <span class="hlt">design</span> procedure for determining the adaptive law's gain matrix. The resulting control algorithm has a guaranteed convergence rate and steady state performance in spite of the uncertainty in the rotor system. Several examples are presented which demonstrate the effectiveness of this approach and its advantages over the standard optimal control formulation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28682269','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28682269"><span>Adaptive Critic Nonlinear <span class="hlt">Robust</span> Control: A Survey.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wang, Ding; He, Haibo; Liu, Derong</p> <p>2017-10-01</p> <p>Adaptive dynamic programming (ADP) and reinforcement learning are quite relevant to each other when performing intelligent optimization. They are both regarded as promising methods involving important components of evaluation and improvement, at the background of information technology, such as artificial intelligence, big data, and deep learning. Although great progresses have been achieved and surveyed when addressing nonlinear optimal control problems, the research on <span class="hlt">robustness</span> of ADP-based control strategies under uncertain environment has not been fully summarized. Hence, this survey reviews the recent main results of adaptive-critic-based <span class="hlt">robust</span> control <span class="hlt">design</span> of continuous-time nonlinear systems. The ADP-based nonlinear optimal regulation is reviewed, followed by <span class="hlt">robust</span> stabilization of nonlinear systems with matched uncertainties, guaranteed cost control <span class="hlt">design</span> of unmatched plants, and decentralized stabilization of interconnected systems. Additionally, further comprehensive discussions are presented, including event-based <span class="hlt">robust</span> control <span class="hlt">design</span>, improvement of the critic learning rule, nonlinear H ∞ control <span class="hlt">design</span>, and several notes on future perspectives. By applying the ADP-based optimal and <span class="hlt">robust</span> control methods to a practical power system and an overhead crane plant, two typical examples are provided to verify the effectiveness of theoretical results. Overall, this survey is beneficial to promote the development of adaptive critic control methods with <span class="hlt">robustness</span> guarantee and the construction of higher level intelligent systems.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA115478','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA115478"><span><span class="hlt">Robust</span> Control Systems.</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>1981-12-01</p> <p>time control system algorithms that will perform adequately (i.e., at least maintain closed-loop system stability) when ucertain parameters in the...system <span class="hlt">design</span> models vary significantly. Such a control algorithm is said to have stability <span class="hlt">robustness</span>-or more simply is said to be "<span class="hlt">robust</span>". This...cas6s above, the performance is analyzed using a covariance analysis. The development of all the controllers and the performance analysis algorithms is</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20040191328','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20040191328"><span>Intelligent, <span class="hlt">Robust</span> Control of Deteriorated Turbofan Engines via Linear Parameter Varying Quadratic Lyapunov Function <span class="hlt">Design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Turso, James A.; Litt, Jonathan S.</p> <p>2004-01-01</p> <p>A method for accommodating engine deterioration via a scheduled Linear Parameter Varying Quadratic Lyapunov Function (LPVQLF)-Based controller is presented. The LPVQLF <span class="hlt">design</span> methodology provides a means for developing unconditionally stable, <span class="hlt">robust</span> control of Linear Parameter Varying (LPV) systems. The controller is scheduled on the Engine Deterioration Index, a function of estimated parameters that relate to engine health, and is computed using a multilayer feedforward neural network. Acceptable thrust response and tight control of exhaust gas temperature (EGT) is accomplished by adjusting the performance weights on these parameters for different levels of engine degradation. Nonlinear simulations demonstrate that the controller achieves specified performance objectives while being <span class="hlt">robust</span> to engine deterioration as well as engine-to-engine variations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23907063','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23907063"><span><span class="hlt">Taguchi</span> approach for co-gasification optimization of torrefied biomass and coal.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Wei-Hsin; Chen, Chih-Jung; Hung, Chen-I</p> <p>2013-09-01</p> <p>This study employs the <span class="hlt">Taguchi</span> method to approach the optimum co-gasification operation of torrefied biomass (eucalyptus) and coal in an entrained flow gasifier. The cold gas efficiency is adopted as the performance index of co-gasification. The influences of six parameters, namely, the biomass blending ratio, oxygen-to-fuel mass ratio (O/F ratio), biomass torrefaction temperature, gasification pressure, steam-to-fuel mass ratio (S/F ratio), and inlet temperature of the carrier gas, on the performance of co-gasification are considered. The analysis of the signal-to-noise ratio suggests that the O/F ratio is the most important factor in determining the performance and the appropriate O/F ratio is 0.7. The performance is also significantly affected by biomass along with torrefaction, where a torrefaction temperature of 300°C is sufficient to upgrade eucalyptus. According to the recommended operating conditions, the values of cold gas efficiency and carbon conversion at the optimum co-gasification are 80.99% and 94.51%, respectively. Copyright © 2013 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28773830','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28773830"><span>Optimization of Injection Molding Parameters for HDPE/TiO₂ Nanocomposites Fabrication with Multiple Performance Characteristics Using the <span class="hlt">Taguchi</span> Method and Grey Relational Analysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Pervez, Hifsa; Mozumder, Mohammad S; Mourad, Abdel-Hamid I</p> <p>2016-08-22</p> <p>The current study presents an investigation on the optimization of injection molding parameters of HDPE/TiO₂ nanocomposites using grey relational analysis with the <span class="hlt">Taguchi</span> method. Four control factors, including filler concentration (i.e., TiO₂), barrel temperature, residence time and holding time, were chosen at three different levels of each. Mechanical properties, such as yield strength, Young's modulus and elongation, were selected as the performance targets. Nine experimental runs were carried out based on the <span class="hlt">Taguchi</span> L₉ orthogonal array, and the data were processed according to the grey relational steps. The optimal process parameters were found based on the average responses of the grey relational grades, and the ideal operating conditions were found to be a filler concentration of 5 wt % TiO₂, a barrel temperature of 225 °C, a residence time of 30 min and a holding time of 20 s. Moreover, analysis of variance (ANOVA) has also been applied to identify the most significant factor, and the percentage of TiO₂ nanoparticles was found to have the most significant effect on the properties of the HDPE/TiO₂ nanocomposites fabricated through the injection molding process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930017718','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930017718"><span><span class="hlt">Robustness</span> enhancement of neurocontroller and state estimator</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Troudet, Terry</p> <p>1993-01-01</p> <p>The feasibility of enhancing neurocontrol <span class="hlt">robustness</span>, through training of the neurocontroller and state estimator in the presence of system uncertainties, is investigated on the example of a multivariable aircraft control problem. The performance and <span class="hlt">robustness</span> of the newly trained neurocontroller are compared to those for an existing neurocontrol <span class="hlt">design</span> scheme. The newly <span class="hlt">designed</span> dynamic neurocontroller exhibits a better trade-off between phase and gain stability margins, and it is significantly more <span class="hlt">robust</span> to degradations of the plant dynamics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2002ApOpt..41.3092V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2002ApOpt..41.3092V"><span><span class="hlt">Design</span> of a <span class="hlt">robust</span> thin-film interference filter for erbium-doped fiber amplifier gain equalization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Verly, Pierre G.</p> <p>2002-06-01</p> <p>Gain-flattening filters (GFFs) are key wavelength division multiplexing components in fiber-optics telecommunications. Challenging issues in the <span class="hlt">design</span> of thin-film GFFs were recently the subject of a contest organized at the 2001 Conference on Optical Interference Coatings. The interest and main difficulty of the proposed problem was to minimize the sensitivity of a GFF to simulated fabrication errors. A high-yield solution and its <span class="hlt">design</span> philosophy are described. The approach used to control the filter <span class="hlt">robustness</span> is explained and illustrated by numerical results.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_16 --> <div id="page_17" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="321"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/12064385','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/12064385"><span><span class="hlt">Design</span> of a <span class="hlt">robust</span> thin-film interference filter for erbium-doped fiber amplifier gain equalization.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Verly, Pierre G</p> <p>2002-06-01</p> <p>Gain-flattening filters (GFFs) are key wavelength division multiplexing components in fiber-optics telecommunications. Challenging issues in the <span class="hlt">design</span> of thin-film GFFs were recently the subject of a contest organized at the 2001 Conference on Optical Interference Coatings. The interest and main difficulty of the proposed problem was to minimize the sensitivity of a GFF to simulated fabrication errors. A high-yield solution and its <span class="hlt">design</span> philosophy are described. The approach used to control the filter <span class="hlt">robustness</span> is explained and illustrated by numerical results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940031406','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940031406"><span><span class="hlt">Robust</span> tracking control of a magnetically suspended rigid body</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lim, Kyong B.; Cox, David E.</p> <p>1994-01-01</p> <p>This study is an application of H-infinity and micro-synthesis for <span class="hlt">designing</span> <span class="hlt">robust</span> tracking controllers for the Large Angle Magnetic Suspension Test Facility. The modeling, <span class="hlt">design</span>, analysis, simulation, and testing of a control law that guarantees tracking performance under external disturbances and model uncertainties is investigated. The type of uncertainties considered and the tracking performance metric used is discussed. This study demonstrates the tradeoff between tracking performance at low frequencies and <span class="hlt">robustness</span> at high frequencies. Two sets of controllers were <span class="hlt">designed</span> and tested. The first set emphasized performance over <span class="hlt">robustness</span>, while the second set traded off performance for <span class="hlt">robustness</span>. Comparisons of simulation and test results are also included. Current simulation and experimental results indicate that reasonably good <span class="hlt">robust</span> tracking performance can be attained for this system using multivariable <span class="hlt">robust</span> control approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MPLB...3240027L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MPLB...3240027L"><span><span class="hlt">Design</span> and operation of a bio-inspired micropump based on blood-sucking mechanism of mosquitoes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Leu, Tzong-Shyng; Kao, Ruei-Hung</p> <p>2018-05-01</p> <p>The study is to develop a novel bionic micropump, mimicking blood-suck mechanism of mosquitos with a similar efficiency of 36%. The micropump is produced by using micro-electro-mechanical system (MEMS) technology, PDMS (polydimethylsiloxane) to fabricate the microchannel, and an actuator membrane made by Fe-PDMS. It employs an Nd-FeB permanent magnet and PZT to actuate the Fe-PDMS membrane for generating flow rate. A lumped model theory and the <span class="hlt">Taguchi</span> method are used for numerical simulation of pulsating flow in the micropump. Also focused is to change the size of mosquito mouth for identifying the best waveform for the transient flow processes. Based on computational results of channel size and the <span class="hlt">Taguchi</span> method, an optimization actuation waveform is identified. The maximum pumping flow rate is 23.5 μL/min and the efficiency is 86%. The power density of micropump is about 8 times of that produced by mosquito’s suction. In addition to using theoretical <span class="hlt">design</span> of the channel size, also combine with <span class="hlt">Taguchi</span> method and asymmetric actuation to find the optimization actuation waveform, the experimental result shows the maximum pumping flowrate is 23.5 μL/min and efficiency is 86%, moreover, the power density of micropump is 8 times higher than mosquito’s.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JIEIC.tmp...12S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JIEIC.tmp...12S"><span>Investigation and <span class="hlt">Taguchi</span> Optimization of Microbial Fuel Cell Salt Bridge Dimensional Parameters</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sarma, Dhrupad; Barua, Parimal Bakul; Dey, Nabendu; Nath, Sumitro; Thakuria, Mrinmay; Mallick, Synthia</p> <p>2018-01-01</p> <p>One major problem of two chamber salt bridge microbial fuel cells (MFCs) is the high resistance offered by the salt bridge to anion flow. Many researchers who have studied and optimized various parameters related to salt bridge MFC, have not shed much light on the effect of salt bridge dimensional parameters on the MFC performance. Therefore, the main objective of this research is to investigate the effect of length and cross sectional area of salt bridge and the effect of solar radiation and atmospheric temperature on MFC current output. An experiment has been <span class="hlt">designed</span> using <span class="hlt">Taguchi</span> L9 orthogonal array, taking length and cross sectional area of salt bridge as factors having three levels. Nine MFCs were fabricated as per the nine trial conditions. Trials were conducted for 3 days and output current of each of the MFCs along with solar insolation and atmospheric temperature were recorded. Analysis of variance shows that salt bridge length has significant effect both on mean (with 53.90% contribution at 95% CL) and variance (with 56.46% contribution at 87% CL), whereas the effect of cross sectional area of the salt bridge and the interaction of these two factors is significant on mean only (with 95% CL). Optimum combination was found at 260 mm salt bridge length and 506.7 mm2 cross sectional area with 4.75 mA of mean output current. The temperature and solar insolation data when correlated with each of the MFCs average output current, revealed that both external factors have significant impact on MFC current output but the correlation coefficient varies from MFC to MFC depending on salt bridge dimensional parameters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJQI...1650004J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJQI...1650004J"><span>Sampled-data <span class="hlt">design</span> for sliding mode control based on various <span class="hlt">robust</span> specifications in open quantum system</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ji, Yinghua; Ju-Ju, Hu; Jian-Hua, Huang; Qiang, Ke</p> <p></p> <p>Due to the influence of decoherence, the quantum state probably evolves from the initial pure state to the mixed state, resulting in loss of fidelity, coherence and purity, which is deteriorating for quantum information transmission. Thus, in quantum engineering, quantum control should not only realize the transfer and track of quantum states through manipulation of the external electromagnetic field but also enhance the <span class="hlt">robustness</span> against decoherence. In this paper, we aim to <span class="hlt">design</span> a control law to steer the system into the sliding mode domain and maintain it in that domain when bounded uncertainties exist in the system Hamiltonian. We first define the required control performance by fidelity, degree of coherence and purity in terms of the uncertainty of the Hamiltonian in Markovian open quantum system. By characterizing the required <span class="hlt">robustness</span> using a sliding mode domain, a sampled-data <span class="hlt">design</span> method is introduced for decoherence control in the quantum system. Furthermore, utilizing the sampled data, a control scheme has been <span class="hlt">designed</span> on the basis of sliding mode control, and the choice of sampling operator and driving of quantum state during the sampling by the Lyapunov control method are discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29373115','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29373115"><span>Active disturbance rejection control based <span class="hlt">robust</span> output feedback autopilot <span class="hlt">design</span> for airbreathing hypersonic vehicles.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tian, Jiayi; Zhang, Shifeng; Zhang, Yinhui; Li, Tong</p> <p>2018-03-01</p> <p>Since motion control plant (y (n) =f(⋅)+d) was repeatedly used to exemplify how active disturbance rejection control (ADRC) works when it was proposed, the integral chain system subject to matched disturbances is always regarded as a canonical form and even misconstrued as the only form that ADRC is applicable to. In this paper, a systematic approach is first presented to apply ADRC to a generic nonlinear uncertain system with mismatched disturbances and a <span class="hlt">robust</span> output feedback autopilot for an airbreathing hypersonic vehicle (AHV) is devised based on that. The key idea is to employ the feedback linearization (FL) and equivalent input disturbance (EID) technique to decouple nonlinear uncertain system into several subsystems in canonical form, thus it would be much easy to directly <span class="hlt">design</span> classical/improved linear/nonlinear ADRC controller for each subsystem. It is noticed that all disturbances are taken into account when implementing FL rather than just omitting that in previous research, which greatly enhances controllers' <span class="hlt">robustness</span> against external disturbances. For autopilot <span class="hlt">design</span>, ADRC strategy enables precise tracking for velocity and altitude reference command in the presence of severe parametric perturbations and atmospheric disturbances only using measurable output information. Bounded-input-bounded-output (BIBO) stable is analyzed for closed-loop system. To illustrate the feasibility and superiority of this novel <span class="hlt">design</span>, a series of comparative simulations with some prominent and representative methods are carried out on a benchmark longitudinal AHV model. Copyright © 2018 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29074375','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29074375"><span>An Intercompany Perspective on Biopharmaceutical Drug Product <span class="hlt">Robustness</span> Studies.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Morar-Mitrica, Sorina; Adams, Monica L; Crotts, George; Wurth, Christine; Ihnat, Peter M; Tabish, Tanvir; Antochshuk, Valentyn; DiLuzio, Willow; Dix, Daniel B; Fernandez, Jason E; Gupta, Kapil; Fleming, Michael S; He, Bing; Kranz, James K; Liu, Dingjiang; Narasimhan, Chakravarthy; Routhier, Eric; Taylor, Katherine D; Truong, Nobel; Stokes, Elaine S E</p> <p>2018-02-01</p> <p>The Biophorum Development Group (BPDG) is an industry-wide consortium enabling networking and sharing of best practices for the development of biopharmaceuticals. To gain a better understanding of current industry approaches for establishing biopharmaceutical drug product (DP) <span class="hlt">robustness</span>, the BPDG-Formulation Point Share group conducted an intercompany collaboration exercise, which included a bench-marking survey and extensive group discussions around the scope, <span class="hlt">design</span>, and execution of <span class="hlt">robustness</span> studies. The results of this industry collaboration revealed several key common themes: (1) overall DP <span class="hlt">robustness</span> is defined by both the formulation and the manufacturing process <span class="hlt">robustness</span>; (2) <span class="hlt">robustness</span> integrates the principles of quality by <span class="hlt">design</span> (QbD); (3) DP <span class="hlt">robustness</span> is an important factor in setting critical quality attribute control strategies and commercial specifications; (4) most companies employ <span class="hlt">robustness</span> studies, along with prior knowledge, risk assessments, and statistics, to develop the DP <span class="hlt">design</span> space; (5) studies are tailored to commercial development needs and the practices of each company. Three case studies further illustrate how a <span class="hlt">robustness</span> study <span class="hlt">design</span> for a biopharmaceutical DP balances experimental complexity, statistical power, scientific understanding, and risk assessment to provide the desired product and process knowledge. The BPDG-Formulation Point Share discusses identified industry challenges with regard to biopharmaceutical DP <span class="hlt">robustness</span> and presents some recommendations for best practices. Copyright © 2018 American Pharmacists Association®. Published by Elsevier Inc. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013NatSR...3E1969S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013NatSR...3E1969S"><span>Towards <span class="hlt">designing</span> <span class="hlt">robust</span> coupled networks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schneider, Christian M.; Yazdani, Nuri; Araújo, Nuno A. M.; Havlin, Shlomo; Herrmann, Hans J.</p> <p>2013-06-01</p> <p>Natural and technological interdependent systems have been shown to be highly vulnerable due to cascading failures and an abrupt collapse of global connectivity under initial failure. Mitigating the risk by partial disconnection endangers their functionality. Here we propose a systematic strategy of selecting a minimum number of autonomous nodes that guarantee a smooth transition in <span class="hlt">robustness</span>. Our method which is based on betweenness is tested on various examples including the famous 2003 electrical blackout of Italy. We show that, with this strategy, the necessary number of autonomous nodes can be reduced by a factor of five compared to a random choice. We also find that the transition to abrupt collapse follows tricritical scaling characterized by a set of exponents which is independent on the protection strategy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017IJSS...48...95P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017IJSS...48...95P"><span><span class="hlt">Robust</span> PI and PID <span class="hlt">design</span> for first- and second-order processes with zeros, time-delay and structured uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Parada, M.; Sbarbaro, D.; Borges, R. A.; Peres, P. L. D.</p> <p>2017-01-01</p> <p>The use of <span class="hlt">robust</span> <span class="hlt">design</span> techniques such as the one based on ? and ? for tuning proportional integral (PI) and proportional integral derivative (PID) controllers have been limited to address a small set of processes. This work addresses the problem by considering a wide set of possible plants, both first- and second-order continuous-time systems with time delays and zeros, leading to PI and PID controllers. The use of structured uncertainties to handle neglected dynamics allows to expand the range of processes to be considered. The proposed approach takes into account the <span class="hlt">robustness</span> of the controller with respect to these structured uncertainties by using the small-gain theorem. In addition, improved performance is sought through the minimisation of an upper bound to the closed-loop system ? norm. A Lyapunov-Krasovskii-type functional is used to obtain delay-dependent <span class="hlt">design</span> conditions. The controller <span class="hlt">design</span> is accomplished by means of a convex optimisation procedure formulated using linear matrix inequalities. In order to illustrate the flexibility of the approach, several examples considering recycle compensation, reduced-order controller <span class="hlt">design</span> and a practical implementation are addressed. Numerical experiments are provided in each case to highlight the main characteristics of the proposed <span class="hlt">design</span> method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006SPIE.6230E..25K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006SPIE.6230E..25K"><span>A <span class="hlt">robust</span> nonlinear skid-steering control <span class="hlt">design</span> applied to the MULE (6x6) unmanned ground vehicle</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kaloust, Joseph</p> <p>2006-05-01</p> <p>The paper presents a <span class="hlt">robust</span> nonlinear skid-steering control <span class="hlt">design</span> concept. The control concept is based on the recursive/backstepping control <span class="hlt">design</span> technique and is capable of compensating for uncertainties associated with sensor noise measurements and/or system dynamic state uncertainties. The objective of this control <span class="hlt">design</span> is to demonstrate the performance of the nonlinear controller under uncertainty associate with road traction (rough off-road and on-road terrain). The MULE vehicle is used in the simulation modeling and results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015IJSyS..46.2258K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015IJSyS..46.2258K"><span><span class="hlt">Robust</span> <span class="hlt">design</span> of (s, S) inventory policy parameters in supply chains with demand and lead time uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Karimi Movahed, Kamran; Zhang, Zhi-Hai</p> <p>2015-09-01</p> <p>Demand and lead time uncertainties have significant effects on supply chain behaviour. In this paper, we present a single-product three-level multi-period supply chain with uncertain demands and lead times by using <span class="hlt">robust</span> techniques to study the managerial insights of the supply chain inventory system under uncertainty. We formulate this problem as a <span class="hlt">robust</span> mixed-integer linear program with minimised expected cost and total cost variation to determine the optimal (s, S) values of the inventory parameters. Several numerical studies are performed to investigate the supply chain behaviour. Useful guidelines for the <span class="hlt">design</span> of a <span class="hlt">robust</span> supply chain are also provided. Results show that the order variance and the expected cost in a supply chain significantly increase when the manufacturer's review period is an integer ratio of the distributor's and the retailer's review periods.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5512532','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5512532"><span>Optimization of Injection Molding Parameters for HDPE/TiO2 Nanocomposites Fabrication with Multiple Performance Characteristics Using the <span class="hlt">Taguchi</span> Method and Grey Relational Analysis</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Pervez, Hifsa; Mozumder, Mohammad S.; Mourad, Abdel-Hamid I.</p> <p>2016-01-01</p> <p>The current study presents an investigation on the optimization of injection molding parameters of HDPE/TiO2 nanocomposites using grey relational analysis with the <span class="hlt">Taguchi</span> method. Four control factors, including filler concentration (i.e., TiO2), barrel temperature, residence time and holding time, were chosen at three different levels of each. Mechanical properties, such as yield strength, Young’s modulus and elongation, were selected as the performance targets. Nine experimental runs were carried out based on the <span class="hlt">Taguchi</span> L9 orthogonal array, and the data were processed according to the grey relational steps. The optimal process parameters were found based on the average responses of the grey relational grades, and the ideal operating conditions were found to be a filler concentration of 5 wt % TiO2, a barrel temperature of 225 °C, a residence time of 30 min and a holding time of 20 s. Moreover, analysis of variance (ANOVA) has also been applied to identify the most significant factor, and the percentage of TiO2 nanoparticles was found to have the most significant effect on the properties of the HDPE/TiO2 nanocomposites fabricated through the injection molding process. PMID:28773830</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015IJSyS..46.2955H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015IJSyS..46.2955H"><span>A <span class="hlt">robust</span> H∞-tracking <span class="hlt">design</span> for uncertain Takagi-Sugeno fuzzy systems with unknown premise variables using descriptor redundancy approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hassan Asemani, Mohammad; Johari Majd, Vahid</p> <p>2015-12-01</p> <p>This paper addresses a <span class="hlt">robust</span> H∞ fuzzy observer-based tracking <span class="hlt">design</span> problem for uncertain Takagi-Sugeno fuzzy systems with external disturbances. To have a practical observer-based controller, the premise variables of the system are assumed to be not measurable in general, which leads to a more complex <span class="hlt">design</span> process. The tracker is synthesised based on a fuzzy Lyapunov function approach and non-parallel distributed compensation (non-PDC) scheme. Using the descriptor redundancy approach, the <span class="hlt">robust</span> stability conditions are derived in the form of strict linear matrix inequalities (LMIs) even in the presence of uncertainties in the system, input, and output matrices simultaneously. Numerical simulations are provided to show the effectiveness of the proposed method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015IJC....88.1429N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015IJC....88.1429N"><span>Hierarchical <span class="hlt">design</span> of an electro-hydraulic actuator based on <span class="hlt">robust</span> LPV methods</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Németh, Balázs; Varga, Balázs; Gáspár, Péter</p> <p>2015-08-01</p> <p>The paper proposes a hierarchical control <span class="hlt">design</span> of an electro-hydraulic actuator, which is used to improve the roll stability of vehicles. The purpose of the control system is to generate a reference torque, which is required by the vehicle dynamic control. The control-oriented model of the actuator is formulated in two subsystems. The high-level hydromotor is described in a linear form, while the low-level spool valve is a polynomial system. These subsystems require different control strategies. At the high level, a linear parameter-varying control is used to guarantee performance specifications. At the low level, a control Lyapunov-function-based algorithm, which creates discrete control input values of the valve, is proposed. The interaction between the two subsystems is guaranteed by the spool displacement, which is control input at the high level and must be tracked at the low-level control. The spool displacement has physical constraints, which must also be incorporated into the control <span class="hlt">design</span>. The <span class="hlt">robust</span> <span class="hlt">design</span> of the high-level control incorporates the imprecision of the low-level control as an uncertainty of the system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MSSP..102..329Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MSSP..102..329Y"><span>Possibility-based <span class="hlt">robust</span> <span class="hlt">design</span> optimization for the structural-acoustic system with fuzzy parameters</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yin, Hui; Yu, Dejie; Yin, Shengwen; Xia, Baizhan</p> <p>2018-03-01</p> <p>The conventional engineering optimization problems considering uncertainties are based on the probabilistic model. However, the probabilistic model may be unavailable because of the lack of sufficient objective information to construct the precise probability distribution of uncertainties. This paper proposes a possibility-based <span class="hlt">robust</span> <span class="hlt">design</span> optimization (PBRDO) framework for the uncertain structural-acoustic system based on the fuzzy set model, which can be constructed by expert opinions. The objective of <span class="hlt">robust</span> <span class="hlt">design</span> is to optimize the expectation and variability of system performance with respect to uncertainties simultaneously. In the proposed PBRDO, the entropy of the fuzzy system response is used as the variability index; the weighted sum of the entropy and expectation of the fuzzy response is used as the objective function, and the constraints are established in the possibility context. The computations for the constraints and objective function of PBRDO are a triple-loop and a double-loop nested problem, respectively, whose computational costs are considerable. To improve the computational efficiency, the target performance approach is introduced to transform the calculation of the constraints into a double-loop nested problem. To further improve the computational efficiency, a Chebyshev fuzzy method (CFM) based on the Chebyshev polynomials is proposed to estimate the objective function, and the Chebyshev interval method (CIM) is introduced to estimate the constraints, thereby the optimization problem is transformed into a single-loop one. Numerical results on a shell structural-acoustic system verify the effectiveness and feasibility of the proposed methods.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016E%26ES...36a2049W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016E%26ES...36a2049W"><span>2-[(Hydroxymethyl)amino]ethanol in water as a preservative: Study of formaldehyde released by <span class="hlt">Taguchi</span>'s method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wisessirikul, W.; Loykulnant, S.; Montha, S.; Fhulua, T.; Prapainainar, P.</p> <p>2016-06-01</p> <p>This research studied the quantity of free formaldehyde released from 2- [(hydroxymethyl)amino]ethanol (HAE) in DI water and natural rubber latex mixture using high-performance liquid chromatography (HPLC) technique. The quantity of formaldehyde retained in the solution was cross-checked by using titration technique. The investigated factors were the concentration of preservative (HAE), pH, and temperature. <span class="hlt">Taguchi</span>'s method was used to <span class="hlt">design</span> the experiments. The number of experiments was reduced to 16 experiments from all possible experiments by orthogonal arrays (3 factors and 4 levels in each factor). Minitab program was used as a tool for statistical calculation and for finding the suitable condition for the preservative system. HPLC studies showed that higher temperature and higher concentration of the preservative influence the amount of formaldehyde released. It was found that conditions at which formaldehyde was released in the lowest amount were 1.6%w/v HAE, 4 to 40 °C, and the original pH. Nevertheless, the pH value of NR latex should be more than 10 (the suitable pH value was found to be 13). This preservative can be used to replace current preservative systems and can maintain the quality of latex for long-term storage. Use of the proposed preservative system was also shown to have reduced impact on the toxicity of the environment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www3.interscience.wiley.com/journal/119016635/abstract','USGSPUBS'); return false;" href="http://www3.interscience.wiley.com/journal/119016635/abstract"><span>Combining band recovery data and Pollock's <span class="hlt">robust</span> <span class="hlt">design</span> to model temporary and permanent emigration</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Lindberg, M.S.; Kendall, W.L.; Hines, J.E.; Anderson, M.G.</p> <p>2001-01-01</p> <p>Capture-recapture models are widely used to estimate demographic parameters of marked populations. Recently, this statistical theory has been extended to modeling dispersal of open populations. Multistate models can be used to estimate movement probabilities among subdivided populations if multiple sites are sampled. Frequently, however, sampling is limited to a single site. Models described by Burnham (1993, in Marked Individuals in the Study of Bird Populations, 199-213), which combined open population capture-recapture and band-recovery models, can be used to estimate permanent emigration when sampling is limited to a single population. Similarly, Kendall, Nichols, and Hines (1997, Ecology 51, 563-578) developed models to estimate temporary emigration under Pollock's (1982, Journal of Wildlife Management 46, 757-760) <span class="hlt">robust</span> <span class="hlt">design</span>. We describe a likelihood-based approach to simultaneously estimate temporary and permanent emigration when sampling is limited to a single population. We use a sampling <span class="hlt">design</span> that combines the <span class="hlt">robust</span> <span class="hlt">design</span> and recoveries of individuals obtained immediately following each sampling period. We present a general form for our model where temporary emigration is a first-order Markov process, and we discuss more restrictive models. We illustrate these models with analysis of data on marked Canvasback ducks. Our analysis indicates that probability of permanent emigration for adult female Canvasbacks was 0.193 (SE = 0.082) and that birds that were present at the study area in year i - 1 had a higher probability of presence in year i than birds that were not present in year i - 1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA597818','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA597818"><span>Improving Large Cetacean Implantable Satellite Tag <span class="hlt">Designs</span> to Maximize Tag <span class="hlt">Robustness</span> and Minimize Health Effects to Individual Animals</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2013-09-30</p> <p><span class="hlt">Designs</span> to Maximize Tag <span class="hlt">Robustness</span> and Minimize Health Effects to Individual Animals Alexandre N. Zerbini Cascadia Research Collective 218 ½ 4th...the blubber-muscle interface and minimize physical and physiological effects of body penetrating tags to individual animals . OBJECTIVES (1...integrity of <span class="hlt">designs</span> created in Objective (1) during laboratory experiments and in cetacean carcasses ; (3) Examine structural tissue damage in the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25942836','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25942836"><span>Influence of process parameters on the content of biomimetic calcium phosphate coating on titanium: a <span class="hlt">Taguchi</span> analysis.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Thammarakcharoen, Faungchat; Suvannapruk, Waraporn; Suwanprateeb, Jintamai</p> <p>2014-10-01</p> <p>In this study, a statistical <span class="hlt">design</span> of experimental methodology based on <span class="hlt">Taguchi</span> orthogonal <span class="hlt">design</span> has been used to study the effect of various processing parameters on the amount of calcium phosphate coating produced by such technique. Seven control factors with three levels each including sodium hydroxide concentration, pretreatment temperature, pretreatment time, cleaning method, coating time, coating temperature and surface area to solution volume ratio were studied. X-ray diffraction revealed that all the coatings consisted of the mixture of octacalcium phosphate (OCP) and hydroxyapatite (HA) and the presence of each phase depended on the process conditions used. Various content and size (-1-100 μm) of isolated spheroid particles with nanosized plate-like morphology deposited on the titanium surface or a continuous layer of plate-like nanocrystals having the plate thickness in the range of -100-300 nm and the plate width in the range of 3-8 μm were formed depending on the process conditions employed. The optimum condition of using sodium hydroxide concentration of 1 M, pretreatment temperature of 70 degrees C, pretreatment time of 24 h, cleaning by ultrasonic, coating time of 6 h, coating temperature of 50 degrees C and surface area to solution volume ratio of 32.74 for producing the greatest amount of the coating formed on the titanium surface was predicted and validated. In addition, coating temperature was found to be the dominant factor with the greatest contribution to the coating formation while coating time and cleaning method were significant factors. Other factors had negligible effects on the coating performance.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19990087092','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19990087092"><span>Metamodels for Computer-Based Engineering <span class="hlt">Design</span>: Survey and Recommendations</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Simpson, Timothy W.; Peplinski, Jesse; Koch, Patrick N.; Allen, Janet K.</p> <p>1997-01-01</p> <p>The use of statistical techniques to build approximations of expensive computer analysis codes pervades much of todays engineering <span class="hlt">design</span>. These statistical approximations, or metamodels, are used to replace the actual expensive computer analyses, facilitating multidisciplinary, multiobjective optimization and concept exploration. In this paper we review several of these techniques including <span class="hlt">design</span> of experiments, response surface methodology, <span class="hlt">Taguchi</span> methods, neural networks, inductive learning, and kriging. We survey their existing application in engineering <span class="hlt">design</span> and then address the dangers of applying traditional statistical techniques to approximate deterministic computer analysis codes. We conclude with recommendations for the appropriate use of statistical approximation techniques in given situations and how common pitfalls can be avoided.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_17 --> <div id="page_18" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="341"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25373790','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25373790"><span>Experimental <span class="hlt">design</span> methods for bioengineering applications.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Keskin Gündoğdu, Tuğba; Deniz, İrem; Çalışkan, Gülizar; Şahin, Erdem Sefa; Azbar, Nuri</p> <p>2016-01-01</p> <p>Experimental <span class="hlt">design</span> is a form of process analysis in which certain factors are selected to obtain the desired responses of interest. It may also be used for the determination of the effects of various independent factors on a dependent factor. The bioengineering discipline includes many different areas of scientific interest, and each study area is affected and governed by many different factors. Briefly analyzing the important factors and selecting an experimental <span class="hlt">design</span> for optimization are very effective tools for the <span class="hlt">design</span> of any bioprocess under question. This review summarizes experimental <span class="hlt">design</span> methods that can be used to investigate various factors relating to bioengineering processes. The experimental methods generally used in bioengineering are as follows: full factorial <span class="hlt">design</span>, fractional factorial <span class="hlt">design</span>, Plackett-Burman <span class="hlt">design</span>, <span class="hlt">Taguchi</span> <span class="hlt">design</span>, Box-Behnken <span class="hlt">design</span> and central composite <span class="hlt">design</span>. These <span class="hlt">design</span> methods are briefly introduced, and then the application of these <span class="hlt">design</span> methods to study different bioengineering processes is analyzed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19870002134&hterms=th&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dth','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19870002134&hterms=th&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dth"><span>A methodology for <span class="hlt">designing</span> <span class="hlt">robust</span> multivariable nonlinear control systems. Ph.D. Thesis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Grunberg, D. B.</p> <p>1986-01-01</p> <p>A new methodology is described for the <span class="hlt">design</span> of nonlinear dynamic controllers for nonlinear multivariable systems providing guarantees of closed-loop stability, performance, and <span class="hlt">robustness</span>. The methodology is an extension of the Linear-Quadratic-Gaussian with Loop-Transfer-Recovery (LQG/LTR) methodology for linear systems, thus hinging upon the idea of constructing an approximate inverse operator for the plant. A major feature of the methodology is a unification of both the state-space and input-output formulations. In addition, new results on stability theory, nonlinear state estimation, and optimal nonlinear regulator theory are presented, including the guaranteed global properties of the extended Kalman filter and optimal nonlinear regulators.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140002367','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140002367"><span><span class="hlt">Robust</span>, Optimal Subsonic Airfoil Shapes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rai, Man Mohan</p> <p>2014-01-01</p> <p>A method has been developed to create an airfoil <span class="hlt">robust</span> enough to operate satisfactorily in different environments. This method determines a <span class="hlt">robust</span>, optimal, subsonic airfoil shape, beginning with an arbitrary initial airfoil shape, and imposes the necessary constraints on the <span class="hlt">design</span>. Also, this method is flexible and extendible to a larger class of requirements and changes in constraints imposed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940010943','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940010943"><span>Research in <span class="hlt">robust</span> control for hypersonic aircraft</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Calise, A. J.</p> <p>1993-01-01</p> <p>The research during the second reporting period has focused on <span class="hlt">robust</span> control <span class="hlt">design</span> for hypersonic vehicles. An already existing <span class="hlt">design</span> for the Hypersonic Winged-Cone Configuration has been enhanced. Uncertainty models for the effects of propulsion system perturbations due to angle of attack variations, structural vibrations, and uncertainty in control effectiveness were developed. Using H(sub infinity) and mu-synthesis techniques, various control <span class="hlt">designs</span> were performed in order to investigate the impact of these effects on achievable <span class="hlt">robust</span> performance.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26410448','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26410448"><span>Application of polynomial control to <span class="hlt">design</span> a <span class="hlt">robust</span> oscillation-damping controller in a multimachine power system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hasanvand, Hamed; Mozafari, Babak; Arvan, Mohammad R; Amraee, Turaj</p> <p>2015-11-01</p> <p>This paper addresses the application of a static Var compensator (SVC) to improve the damping of interarea oscillations. Optimal location and size of SVC are defined using bifurcation and modal analysis to satisfy its primary application. Furthermore, the best-input signal for damping controller is selected using Hankel singular values and right half plane-zeros. The proposed approach is aimed to <span class="hlt">design</span> a <span class="hlt">robust</span> PI controller based on interval plants and Kharitonov's theorem. The objective here is to determine the stability region to attain <span class="hlt">robust</span> stability, the desired phase margin, gain margin, and bandwidth. The intersection of the resulting stability regions yields the set of kp-ki parameters. In addition, optimal multiobjective <span class="hlt">design</span> of PI controller using particle swarm optimization (PSO) algorithm is presented. The effectiveness of the suggested controllers in damping of local and interarea oscillation modes of a multimachine power system, over a wide range of loading conditions and system configurations, is confirmed through eigenvalue analysis and nonlinear time domain simulation. Copyright © 2015 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25524647','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25524647"><span><span class="hlt">Robust</span> enzyme <span class="hlt">design</span>: bioinformatic tools for improved protein stability.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Suplatov, Dmitry; Voevodin, Vladimir; Švedas, Vytas</p> <p>2015-03-01</p> <p>The ability of proteins and enzymes to maintain a functionally active conformation under adverse environmental conditions is an important feature of biocatalysts, vaccines, and biopharmaceutical proteins. From an evolutionary perspective, <span class="hlt">robust</span> stability of proteins improves their biological fitness and allows for further optimization. Viewed from an industrial perspective, enzyme stability is crucial for the practical application of enzymes under the required reaction conditions. In this review, we analyze bioinformatic-driven strategies that are used to predict structural changes that can be applied to wild type proteins in order to produce more stable variants. The most commonly employed techniques can be classified into stochastic approaches, empirical or systematic rational <span class="hlt">design</span> strategies, and <span class="hlt">design</span> of chimeric proteins. We conclude that bioinformatic analysis can be efficiently used to study large protein superfamilies systematically as well as to predict particular structural changes which increase enzyme stability. Evolution has created a diversity of protein properties that are encoded in genomic sequences and structural data. Bioinformatics has the power to uncover this evolutionary code and provide a reproducible selection of hotspots - key residues to be mutated in order to produce more stable and functionally diverse proteins and enzymes. Further development of systematic bioinformatic procedures is needed to organize and analyze sequences and structures of proteins within large superfamilies and to link them to function, as well as to provide knowledge-based predictions for experimental evaluation. Copyright © 2014 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4627627','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4627627"><span><span class="hlt">Design</span> and Evaluation of a <span class="hlt">Robust</span> PID Controller for a Fully Implantable Artificial Pancreas</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2015-01-01</p> <p>Treatment of type 1 diabetes mellitus could be greatly improved by applying a closed-loop control strategy to insulin delivery, also known as an artificial pancreas (AP). In this work, we outline the <span class="hlt">design</span> of a fully implantable AP using intraperitoneal (IP) insulin delivery and glucose sensing. The <span class="hlt">design</span> process utilizes the rapid glucose sensing and insulin action offered by the IP space to tune a PID controller with insulin feedback to provide safe and effective insulin delivery. The controller was tuned to meet <span class="hlt">robust</span> performance and stability specifications. An anti-reset windup strategy was introduced to prevent dangerous undershoot toward hypoglycemia after a large meal disturbance. The final controller <span class="hlt">design</span> achieved 78% of time within the tight glycemic range of 80–140 mg/dL, with no time spent in hypoglycemia. The next step is to test this controller <span class="hlt">design</span> in an animal model to evaluate the in vivo performance. PMID:26538805</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1806n0002L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1806n0002L"><span>A <span class="hlt">robust</span> approach to optimal matched filter <span class="hlt">design</span> in ultrasonic non-destructive evaluation (NDE)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Minghui; Hayward, Gordon</p> <p>2017-02-01</p> <p>The matched filter was demonstrated to be a powerful yet efficient technique to enhance defect detection and imaging in ultrasonic non-destructive evaluation (NDE) of coarse grain materials, provided that the filter was properly <span class="hlt">designed</span> and optimized. In the literature, in order to accurately approximate the defect echoes, the <span class="hlt">design</span> utilized the real excitation signals, which made it time consuming and less straightforward to implement in practice. In this paper, we present a more <span class="hlt">robust</span> and flexible approach to optimal matched filter <span class="hlt">design</span> using the simulated excitation signals, and the control parameters are chosen and optimized based on the real scenario of array transducer, transmitter-receiver system response, and the test sample, as a result, the filter response is optimized and depends on the material characteristics. Experiments on industrial samples are conducted and the results confirm the great benefits of the method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24751476','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24751476"><span><span class="hlt">Robust</span> fault-tolerant tracking control <span class="hlt">design</span> for spacecraft under control input saturation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bustan, Danyal; Pariz, Naser; Sani, Seyyed Kamal Hosseini</p> <p>2014-07-01</p> <p>In this paper, a continuous globally stable tracking control algorithm is proposed for a spacecraft in the presence of unknown actuator failure, control input saturation, uncertainty in inertial matrix and external disturbances. The <span class="hlt">design</span> method is based on variable structure control and has the following properties: (1) fast and accurate response in the presence of bounded disturbances; (2) <span class="hlt">robust</span> to the partial loss of actuator effectiveness; (3) explicit consideration of control input saturation; and (4) <span class="hlt">robust</span> to uncertainty in inertial matrix. In contrast to traditional fault-tolerant control methods, the proposed controller does not require knowledge of the actuator faults and is implemented without explicit fault detection and isolation processes. In the proposed controller a single parameter is adjusted dynamically in such a way that it is possible to prove that both attitude and angular velocity errors will tend to zero asymptotically. The stability proof is based on a Lyapunov analysis and the properties of the singularity free quaternion representation of spacecraft dynamics. Results of numerical simulations state that the proposed controller is successful in achieving high attitude performance in the presence of external disturbances, actuator failures, and control input saturation. Copyright © 2014 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014RJPCA..88.1241G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014RJPCA..88.1241G"><span>Preparation of photocatalytic ZnO nanoparticles and application in photochemical degradation of betamethasone sodium phosphate using <span class="hlt">taguchi</span> approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Giahi, M.; Farajpour, G.; Taghavi, H.; Shokri, S.</p> <p>2014-07-01</p> <p>In this study, ZnO nanoparticles were prepared by a sol-gel method for the first time. <span class="hlt">Taguchi</span> method was used to identify the several factors that may affect degradation percentage of betamethasone sodium phosphate in wastewater in UV/K2S2O8/nano-ZnO system. Our experimental <span class="hlt">design</span> consisted of testing five factors, i.e., dosage of K2S2O8, concentration of betamethasone sodium phosphate, amount of ZnO, irradiation time and initial pH. With four levels of each factor tested. It was found that, optimum parameters are irradiation time, 180 min; pH 9.0; betamethasone sodium phosphate, 30 mg/L; amount of ZnO, 13 mg; K2S2O8, 1 mM. The percentage contribution of each factor was determined by the analysis of variance (ANOVA). The results showed that irradiation time; pH; amount of ZnO; drug concentration and dosage of K2S2O8 contributed by 46.73, 28.56, 11.56, 6.70, and 6.44%, respectively. Finally, the kinetics process was studied and the photodegradation rate of betamethasone sodium phosphate was found to obey pseudo-first-order kinetics equation represented by the Langmuir-Hinshelwood model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21428503','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21428503"><span>Virtual sensors for active noise control in acoustic-structural coupled enclosures using structural sensing: <span class="hlt">robust</span> virtual sensor <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Halim, Dunant; Cheng, Li; Su, Zhongqing</p> <p>2011-03-01</p> <p>The work was aimed to develop a <span class="hlt">robust</span> virtual sensing <span class="hlt">design</span> methodology for sensing and active control applications of vibro-acoustic systems. The proposed virtual sensor was <span class="hlt">designed</span> to estimate a broadband acoustic interior sound pressure using structural sensors, with <span class="hlt">robustness</span> against certain dynamic uncertainties occurring in an acoustic-structural coupled enclosure. A convex combination of Kalman sub-filters was used during the <span class="hlt">design</span>, accommodating different sets of perturbed dynamic model of the vibro-acoustic enclosure. A minimax optimization problem was set up to determine an optimal convex combination of Kalman sub-filters, ensuring an optimal worst-case virtual sensing performance. The virtual sensing and active noise control performance was numerically investigated on a rectangular panel-cavity system. It was demonstrated that the proposed virtual sensor could accurately estimate the interior sound pressure, particularly the one dominated by cavity-controlled modes, by using a structural sensor. With such a virtual sensing technique, effective active noise control performance was also obtained even for the worst-case dynamics. © 2011 Acoustical Society of America</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930003212','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930003212"><span>An advancing front Delaunay triangulation algorithm <span class="hlt">designed</span> for <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mavriplis, D. J.</p> <p>1992-01-01</p> <p>A new algorithm is described for generating an unstructured mesh about an arbitrary two-dimensional configuration. Mesh points are generated automatically by the algorithm in a manner which ensures a smooth variation of elements, and the resulting triangulation constitutes the Delaunay triangulation of these points. The algorithm combines the mathematical elegance and efficiency of Delaunay triangulation algorithms with the desirable point placement features, boundary integrity, and <span class="hlt">robustness</span> traditionally associated with advancing-front-type mesh generation strategies. The method offers increased <span class="hlt">robustness</span> over previous algorithms in that it cannot fail regardless of the initial boundary point distribution and the prescribed cell size distribution throughout the flow-field.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://rcin.org.pl/dlibra/docmetadata?id=11103','USGSPUBS'); return false;" href="http://rcin.org.pl/dlibra/docmetadata?id=11103"><span>The use of a <span class="hlt">robust</span> capture-recapture <span class="hlt">design</span> in small mammal population studies: A field example with Microtus pennsylvanicus</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Nichols, James D.; Pollock, Kenneth H.; Hines, James E.</p> <p>1984-01-01</p> <p>The <span class="hlt">robust</span> <span class="hlt">design</span> of Pollock (1982) was used to estimate parameters of a Maryland M. pennsylvanicus population. Closed model tests provided strong evidence of heterogeneity of capture probability, and model M eta (Otis et al., 1978) was selected as the most appropriate model for estimating population size. The Jolly-Seber model goodness-of-fit test indicated rejection of the model for this data set, and the M eta estimates of population size were all higher than the Jolly-Seber estimates. Both of these results are consistent with the evidence of heterogeneous capture probabilities. The authors thus used M eta estimates of population size, Jolly-Seber estimates of survival rate, and estimates of birth-immigration based on a combination of the population size and survival rate estimates. Advantages of the <span class="hlt">robust</span> <span class="hlt">design</span> estimates for certain inference procedures are discussed, and the <span class="hlt">design</span> is recommended for future small mammal capture-recapture studies directed at estimation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010063955','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010063955"><span>Two Reconfigurable Flight-Control <span class="hlt">Design</span> Methods: <span class="hlt">Robust</span> Servomechanism and Control Allocation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Burken, John J.; Lu, Ping; Wu, Zheng-Lu; Bahm, Cathy</p> <p>2001-01-01</p> <p>Two methods for control system reconfiguration have been investigated. The first method is a <span class="hlt">robust</span> servomechanism control approach (optimal tracking problem) that is a generalization of the classical proportional-plus-integral control to multiple input-multiple output systems. The second method is a control-allocation approach based on a quadratic programming formulation. A globally convergent fixed-point iteration algorithm has been developed to make onboard implementation of this method feasible. These methods have been applied to reconfigurable entry flight control <span class="hlt">design</span> for the X-33 vehicle. Examples presented demonstrate simultaneous tracking of angle-of-attack and roll angle commands during failures of the fight body flap actuator. Although simulations demonstrate success of the first method in most cases, the control-allocation method appears to provide uniformly better performance in all cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3508828','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3508828"><span>Different <span class="hlt">designs</span> of kinase-phosphatase interactions and phosphatase sequestration shapes the <span class="hlt">robustness</span> and signal flow in the MAPK cascade</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2012-01-01</p> <p>Background The three layer mitogen activated protein kinase (MAPK) signaling cascade exhibits different <span class="hlt">designs</span> of interactions between its kinases and phosphatases. While the sequential interactions between the three kinases of the cascade are tightly preserved, the phosphatases of the cascade, such as MKP3 and PP2A, exhibit relatively diverse interactions with their substrate kinases. Additionally, the kinases of the MAPK cascade can also sequester their phosphatases. Thus, each topologically distinct interaction <span class="hlt">design</span> of kinases and phosphatases could exhibit unique signal processing characteristics, and the presence of phosphatase sequestration may lead to further fine tuning of the propagated signal. Results We have built four architecturally distinct types of models of the MAPK cascade, each model with identical kinase-kinase interactions but unique kinases-phosphatases interactions. Our simulations unravelled that MAPK cascade’s <span class="hlt">robustness</span> to external perturbations is a function of nature of interaction between its kinases and phosphatases. The cascade’s output <span class="hlt">robustness</span> was enhanced when phosphatases were sequestrated by their target kinases. We uncovered a novel implicit/hidden negative feedback loop from the phosphatase MKP3 to its upstream kinase Raf-1, in a cascade resembling the B cell MAPK cascade. Notably, strength of the feedback loop was reciprocal to the strength of phosphatases’ sequestration and stronger sequestration abolished the feedback loop completely. An experimental method to verify the presence of the feedback loop is also proposed. We further showed, when the models were activated by transient signal, memory (total time taken by the cascade output to reach its unstimulated level after removal of signal) of a cascade was determined by the specific <span class="hlt">designs</span> of interaction among its kinases and phosphatases. Conclusions Differences in interaction <span class="hlt">designs</span> among the kinases and phosphatases can differentially shape the <span class="hlt">robustness</span> and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22315563','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22315563"><span>Real-time PCR machine system modeling and a systematic approach for the <span class="hlt">robust</span> <span class="hlt">design</span> of a real-time PCR-on-a-chip system.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lee, Da-Sheng</p> <p>2010-01-01</p> <p>Chip-based DNA quantification systems are widespread, and used in many point-of-care applications. However, instruments for such applications may not be maintained or calibrated regularly. Since machine reliability is a key issue for normal operation, this study presents a system model of the real-time Polymerase Chain Reaction (PCR) machine to analyze the instrument <span class="hlt">design</span> through numerical experiments. Based on model analysis, a systematic approach was developed to lower the variation of DNA quantification and achieve a <span class="hlt">robust</span> <span class="hlt">design</span> for a real-time PCR-on-a-chip system. Accelerated lift testing was adopted to evaluate the reliability of the chip prototype. According to the life test plan, this proposed real-time PCR-on-a-chip system was simulated to work continuously for over three years with similar reproducibility in DNA quantification. This not only shows the <span class="hlt">robustness</span> of the lab-on-a-chip system, but also verifies the effectiveness of our systematic method for achieving a <span class="hlt">robust</span> <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3270864','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3270864"><span>Real-time PCR Machine System Modeling and a Systematic Approach for the <span class="hlt">Robust</span> <span class="hlt">Design</span> of a Real-time PCR-on-a-Chip System</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lee, Da-Sheng</p> <p>2010-01-01</p> <p>Chip-based DNA quantification systems are widespread, and used in many point-of-care applications. However, instruments for such applications may not be maintained or calibrated regularly. Since machine reliability is a key issue for normal operation, this study presents a system model of the real-time Polymerase Chain Reaction (PCR) machine to analyze the instrument <span class="hlt">design</span> through numerical experiments. Based on model analysis, a systematic approach was developed to lower the variation of DNA quantification and achieve a <span class="hlt">robust</span> <span class="hlt">design</span> for a real-time PCR-on-a-chip system. Accelerated lift testing was adopted to evaluate the reliability of the chip prototype. According to the life test plan, this proposed real-time PCR-on-a-chip system was simulated to work continuously for over three years with similar reproducibility in DNA quantification. This not only shows the <span class="hlt">robustness</span> of the lab-on-a-chip system, but also verifies the effectiveness of our systematic method for achieving a <span class="hlt">robust</span> <span class="hlt">design</span>. PMID:22315563</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA452020','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA452020"><span>Optimization-Based <span class="hlt">Robust</span> Nonlinear Control</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2006-08-01</p> <p>ABSTRACT New control algorithms were developed for <span class="hlt">robust</span> stabilization of nonlinear dynamical systems . Novel, linear matrix inequality-based synthesis...was to further advance optimization-based <span class="hlt">robust</span> nonlinear control <span class="hlt">design</span>, for general nonlinear systems (especially in discrete time ), for linear...Teel, IEEE Transactions on Control Systems Technology, vol. 14, no. 3, p. 398-407, May 2006. 3. "A unified framework for input-to-state stability in</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22109441','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22109441"><span><span class="hlt">Robust</span> holographic storage system <span class="hlt">design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Watanabe, Takahiro; Watanabe, Minoru</p> <p>2011-11-21</p> <p>Demand is increasing daily for large data storage systems that are useful for applications in spacecraft, space satellites, and space robots, which are all exposed to radiation-rich space environment. As candidates for use in space embedded systems, holographic storage systems are promising because they can easily provided the demanded large-storage capability. Particularly, holographic storage systems, which have no rotation mechanism, are demanded because they are virtually maintenance-free. Although a holographic memory itself is an extremely <span class="hlt">robust</span> device even in a space radiation environment, its associated lasers and drive circuit devices are vulnerable. Such vulnerabilities sometimes engendered severe problems that prevent reading of all contents of the holographic memory, which is a turn-off failure mode of a laser array. This paper therefore presents a proposal for a recovery method for the turn-off failure mode of a laser array on a holographic storage system, and describes results of an experimental demonstration. © 2011 Optical Society of America</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030014504','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030014504"><span>Options for <span class="hlt">Robust</span> Airfoil Optimization under Uncertainty</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Padula, Sharon L.; Li, Wu</p> <p>2002-01-01</p> <p>A <span class="hlt">robust</span> optimization method is developed to overcome point-optimization at the sampled <span class="hlt">design</span> points. This method combines the best features from several preliminary methods proposed by the authors and their colleagues. The <span class="hlt">robust</span> airfoil shape optimization is a direct method for drag reduction over a given range of operating conditions and has three advantages: (1) it prevents severe degradation in the off-<span class="hlt">design</span> performance by using a smart descent direction in each optimization iteration, (2) it uses a large number of spline control points as <span class="hlt">design</span> variables yet the resulting airfoil shape does not need to be smoothed, and (3) it allows the user to make a tradeoff between the level of optimization and the amount of computing time consumed. For illustration purposes, the <span class="hlt">robust</span> optimization method is used to solve a lift-constrained drag minimization problem for a two-dimensional (2-D) airfoil in Euler flow with 20 geometric <span class="hlt">design</span> variables.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_18 --> <div id="page_19" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="361"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AcMSn..33..963C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AcMSn..33..963C"><span>Integration of uniform <span class="hlt">design</span> and quantum-behaved particle swarm optimization to the <span class="hlt">robust</span> <span class="hlt">design</span> for a railway vehicle suspension system under different wheel conicities and wheel rolling radii</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cheng, Yung-Chang; Lee, Cheng-Kang</p> <p>2017-10-01</p> <p>This paper proposes a systematic method, integrating the uniform <span class="hlt">design</span> (UD) of experiments and quantum-behaved particle swarm optimization (QPSO), to solve the problem of a <span class="hlt">robust</span> <span class="hlt">design</span> for a railway vehicle suspension system. Based on the new nonlinear creep model derived from combining Hertz contact theory, Kalker's linear theory and a heuristic nonlinear creep model, the modeling and dynamic analysis of a 24 degree-of-freedom railway vehicle system were investigated. The Lyapunov indirect method was used to examine the effects of suspension parameters, wheel conicities and wheel rolling radii on critical hunting speeds. Generally, the critical hunting speeds of a vehicle system resulting from worn wheels with different wheel rolling radii are lower than those of a vehicle system having original wheels without different wheel rolling radii. Because of worn wheels, the critical hunting speed of a running railway vehicle substantially declines over the long term. For safety reasons, it is necessary to <span class="hlt">design</span> the suspension system parameters to increase the <span class="hlt">robustness</span> of the system and decrease the sensitive of wheel noises. By applying UD and QPSO, the nominal-the-best signal-to-noise ratio of the system was increased from -48.17 to -34.05 dB. The rate of improvement was 29.31%. This study has demonstrated that the integration of UD and QPSO can successfully reveal the optimal solution of suspension parameters for solving the <span class="hlt">robust</span> <span class="hlt">design</span> problem of a railway vehicle suspension system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4208167','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4208167"><span>Optimization of an Optical Inspection System Based on the <span class="hlt">Taguchi</span> Method for Quantitative Analysis of Point-of-Care Testing</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Yeh, Chia-Hsien; Zhao, Zi-Qi; Shen, Pi-Lan; Lin, Yu-Cheng</p> <p>2014-01-01</p> <p>This study presents an optical inspection system for detecting a commercial point-of-care testing product and a new detection model covering from qualitative to quantitative analysis. Human chorionic gonadotropin (hCG) strips (cut-off value of the hCG commercial product is 25 mIU/mL) were the detection target in our study. We used a complementary metal-oxide semiconductor (CMOS) sensor to detect the colors of the test line and control line in the specific strips and to reduce the observation errors by the naked eye. To achieve better linearity between the grayscale and the concentration, and to decrease the standard deviation (increase the signal to noise ratio, S/N), the <span class="hlt">Taguchi</span> method was used to find the optimal parameters for the optical inspection system. The pregnancy test used the principles of the lateral flow immunoassay, and the colors of the test and control line were caused by the gold nanoparticles. Because of the sandwich immunoassay model, the color of the gold nanoparticles in the test line was darkened by increasing the hCG concentration. As the results reveal, the S/N increased from 43.48 dB to 53.38 dB, and the hCG concentration detection increased from 6.25 to 50 mIU/mL with a standard deviation of less than 10%. With the optimal parameters to decrease the detection limit and to increase the linearity determined by the <span class="hlt">Taguchi</span> method, the optical inspection system can be applied to various commercial rapid tests for the detection of ketamine, troponin I, and fatty acid binding protein (FABP). PMID:25256108</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=231390&keyword=biometric&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50','EPA-EIMS'); return false;" href="https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=231390&keyword=biometric&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50"><span>DETERMINING A <span class="hlt">ROBUST</span> D-OPTIMAL <span class="hlt">DESIGN</span> FOR TESTING FOR DEPARTURE FROM ADDITIVITY IN A MIXTURE OF FOUR PFAAS</span></a></p> <p><a target="_blank" href="http://oaspub.epa.gov/eims/query.page">EPA Science Inventory</a></p> <p></p> <p></p> <p>Our objective was to determine an optimal experimental <span class="hlt">design</span> for a mixture of perfluoroalkyl acids (PFAAs) that is <span class="hlt">robust</span> to the assumption of additivity. Of particular focus to this research project is whether an environmentally relevant mixture of four PFAAs with long half-liv...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25872221','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25872221"><span>Reinforcement-Learning-Based <span class="hlt">Robust</span> Controller <span class="hlt">Design</span> for Continuous-Time Uncertain Nonlinear Systems Subject to Input Constraints.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Liu, Derong; Yang, Xiong; Wang, Ding; Wei, Qinglai</p> <p>2015-07-01</p> <p>The <span class="hlt">design</span> of stabilizing controller for uncertain nonlinear systems with control constraints is a challenging problem. The constrained-input coupled with the inability to identify accurately the uncertainties motivates the <span class="hlt">design</span> of stabilizing controller based on reinforcement-learning (RL) methods. In this paper, a novel RL-based <span class="hlt">robust</span> adaptive control algorithm is developed for a class of continuous-time uncertain nonlinear systems subject to input constraints. The <span class="hlt">robust</span> control problem is converted to the constrained optimal control problem with appropriately selecting value functions for the nominal system. Distinct from typical action-critic dual networks employed in RL, only one critic neural network (NN) is constructed to derive the approximate optimal control. Meanwhile, unlike initial stabilizing control often indispensable in RL, there is no special requirement imposed on the initial control. By utilizing Lyapunov's direct method, the closed-loop optimal control system and the estimated weights of the critic NN are proved to be uniformly ultimately bounded. In addition, the derived approximate optimal control is verified to guarantee the uncertain nonlinear system to be stable in the sense of uniform ultimate boundedness. Two simulation examples are provided to illustrate the effectiveness and applicability of the present approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PhRvE..91d2813M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PhRvE..91d2813M"><span><span class="hlt">Robustness</span> of spatial micronetworks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>McAndrew, Thomas C.; Danforth, Christopher M.; Bagrow, James P.</p> <p>2015-04-01</p> <p>Power lines, roadways, pipelines, and other physical infrastructure are critical to modern society. These structures may be viewed as spatial networks where geographic distances play a role in the functionality and construction cost of links. Traditionally, studies of network <span class="hlt">robustness</span> have primarily considered the connectedness of large, random networks. Yet for spatial infrastructure, physical distances must also play a role in network <span class="hlt">robustness</span>. Understanding the <span class="hlt">robustness</span> of small spatial networks is particularly important with the increasing interest in microgrids, i.e., small-area distributed power grids that are well suited to using renewable energy resources. We study the random failures of links in small networks where functionality depends on both spatial distance and topological connectedness. By introducing a percolation model where the failure of each link is proportional to its spatial length, we find that when failures depend on spatial distances, networks are more fragile than expected. Accounting for spatial effects in both construction and <span class="hlt">robustness</span> is important for <span class="hlt">designing</span> efficient microgrids and other network infrastructure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5758948','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5758948"><span>Modeling and Multiresponse Optimization for Anaerobic Codigestion of Oil Refinery Wastewater and Chicken Manure by Using Artificial Neural Network and the <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Hemmat, Abbas; Kafashan, Jalal; Huang, Hongying</p> <p>2017-01-01</p> <p>To study the optimum process conditions for pretreatments and anaerobic codigestion of oil refinery wastewater (ORWW) with chicken manure, L9 (34) <span class="hlt">Taguchi</span>'s orthogonal array was applied. The biogas production (BGP), biomethane content (BMP), and chemical oxygen demand solubilization (CODS) in stabilization rate were evaluated as the process outputs. The optimum conditions were obtained by using <span class="hlt">Design</span> Expert software (Version 7.0.0). The results indicated that the optimum conditions could be achieved with 44% ORWW, 36°C temperature, 30 min sonication, and 6% TS in the digester. The optimum BGP, BMP, and CODS removal rates by using the optimum conditions were 294.76 mL/gVS, 151.95 mL/gVS, and 70.22%, respectively, as concluded by the experimental results. In addition, the artificial neural network (ANN) technique was implemented to develop an ANN model for predicting BGP yield and BMP content. The Levenberg-Marquardt algorithm was utilized to train ANN, and the architecture of 9-19-2 for the ANN model was obtained. PMID:29441352</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMGC14A..01S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMGC14A..01S"><span><span class="hlt">Robust</span> Engineering <span class="hlt">Designs</span> for Infrastructure Adaptation to a Changing Climate</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Samaras, C.; Cook, L.</p> <p>2015-12-01</p> <p>Infrastructure systems are expected to be functional, durable and safe over long service lives - 50 to over 100 years. Observations and models of climate science show that greenhouse gas emissions resulting from human activities have changed climate, weather and extreme events. Projections of future changes (albeit with uncertainties caused by inadequacies of current climate/weather models) can be made based on scenarios for future emissions, but actual future emissions are themselves uncertain. Most current engineering standards and practices for infrastructure assume that the probabilities of future extreme climate and weather events will match those of the past. Climate science shows that this assumption is invalid, but is unable, at present, to define these probabilities over the service lives of existing and new infrastructure systems. Engineering <span class="hlt">designs</span>, plans, and institutions and regulations will need to be adaptable for a range of future conditions (conditions of climate, weather and extreme events, as well as changing societal demands for infrastructure services). For their current and future projects, engineers should: Involve all stakeholders (owners, financers, insurance, regulators, affected public, climate/weather scientists, etc.) in key decisions; Use low regret, adaptive strategies, such as <span class="hlt">robust</span> decision making and the observational method, comply with relevant standards and regulations, and exceed their requirements where appropriate; Publish <span class="hlt">design</span> studies and performance/failure investigations to extend the body of knowledge for advancement of practice. The engineering community should conduct observational and modeling research with climate/weather/social scientists and the concerned communities and account rationally for climate change in revised engineering standards and codes. This presentation presents initial research on decisionmaking under uncertainty for climate resilient infrastructure <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017IJSS...48.2368S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017IJSS...48.2368S"><span>Real-time control systems: feedback, scheduling and <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Simon, Daniel; Seuret, Alexandre; Sename, Olivier</p> <p>2017-08-01</p> <p>The efficient control of real-time distributed systems, where continuous components are governed through digital devices and communication networks, needs a careful examination of the constraints arising from the different involved domains inside co-<span class="hlt">design</span> approaches. Thanks to the <span class="hlt">robustness</span> of feedback control, both new control methodologies and slackened real-time scheduling schemes are proposed beyond the frontiers between these traditionally separated fields. A methodology to <span class="hlt">design</span> <span class="hlt">robust</span> aperiodic controllers is provided, where the sampling interval is considered as a control variable of the system. Promising experimental results are provided to show the feasibility and <span class="hlt">robustness</span> of the approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.803a2185Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.803a2185Z"><span><span class="hlt">Design</span> of <span class="hlt">robust</span> systems by means of the numerical optimization with harmonic changing of the model parameters</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhmud, V. A.; Reva, I. L.; Dimitrov, L. V.</p> <p>2017-01-01</p> <p>The <span class="hlt">design</span> of <span class="hlt">robust</span> feedback systems by means of the numerical optimization method is mostly accomplished with modeling of the several systems simultaneously. In each such system, regulators are similar. But the object models are different. It includes all edge values from the possible variants of the object model parameters. With all this, not all possible sets of model parameters are taken into account. Hence, the regulator can be not <span class="hlt">robust</span>, i. e. it can not provide system stability in some cases, which were not tested during the optimization procedure. The paper proposes an alternative method. It consists in sequent changing of all parameters according to harmonic low. The frequencies of changing of each parameter are aliquant. It provides full covering of the parameters space.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/12071255','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/12071255"><span>Identification and <span class="hlt">robust</span> control of an experimental servo motor.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Adam, E J; Guestrin, E D</p> <p>2002-04-01</p> <p>In this work, the <span class="hlt">design</span> of a <span class="hlt">robust</span> controller for an experimental laboratory-scale position control system based on a dc motor drive as well as the corresponding identification and <span class="hlt">robust</span> stability analysis are presented. In order to carry out the <span class="hlt">robust</span> <span class="hlt">design</span> procedure, first, a classic closed-loop identification technique is applied and then, the parametrization by internal model control is used. The model uncertainty is evaluated under both parametric and global representation. For the latter case, an interesting discussion about the conservativeness of this description is presented by means of a comparison between the uncertainty disk and the critical perturbation radius approaches. Finally, conclusions about the performance of the experimental system with the <span class="hlt">robust</span> controller are discussed using comparative graphics of the controlled variable and the Nyquist stability margin as a <span class="hlt">robustness</span> measurement.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013EnOp...45..245A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013EnOp...45..245A"><span><span class="hlt">Robust</span> optimization of front members in a full frontal car impact</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aspenberg (né Lönn), David; Jergeus, Johan; Nilsson, Larsgunnar</p> <p>2013-03-01</p> <p>In the search for lightweight automobile <span class="hlt">designs</span>, it is necessary to assure that <span class="hlt">robust</span> crashworthiness performance is achieved. Structures that are optimized to handle a finite number of load cases may perform poorly when subjected to various dispersions. Thus, uncertainties must be accounted for in the optimization process. This article presents an approach to optimization where all <span class="hlt">design</span> evaluations include an evaluation of the <span class="hlt">robustness</span>. Metamodel approximations are applied both to the <span class="hlt">design</span> space and the <span class="hlt">robustness</span> evaluations, using artifical neural networks and polynomials, respectively. The features of the <span class="hlt">robust</span> optimization approach are displayed in an analytical example, and further demonstrated in a large-scale <span class="hlt">design</span> example of front side members of a car. Different optimization formulations are applied and it is shown that the proposed approach works well. It is also concluded that a <span class="hlt">robust</span> optimization puts higher demands on the finite element model performance than normally.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20150009958','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20150009958"><span>Generation After Next Propulsor Research: <span class="hlt">Robust</span> <span class="hlt">Design</span> for Embedded Engine Systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Arend, David J.; Tillman, Gregory; O'Brien, Walter F.</p> <p>2012-01-01</p> <p>The National Aeronautics and Space Administration, United Technologies Research Center and Virginia Polytechnic and State University have contracted to pursue multi-disciplinary research into boundary layer ingesting (BLI) propulsors for generation after next environmentally responsible subsonic fixed wing aircraft. This <span class="hlt">Robust</span> <span class="hlt">Design</span> for Embedded Engine Systems project first conducted a high-level vehicle system study based on a large commercial transport class hybrid wing body aircraft, which determined that a 3 to 5 percent reduction in fuel burn could be achieved over a 7,500 nanometer mission. Both pylon-mounted baseline and BLI propulsion systems were based on a low-pressure-ratio fan (1.35) in an ultra-high-bypass ratio engine (16), consistent with the next generation of advanced commercial turbofans. An optimized, coupled BLI inlet and fan system was subsequently <span class="hlt">designed</span> to achieve performance targets identified in the system study. The resulting system possesses an inlet with total pressure losses less than 0.5%, and a fan stage with an efficiency debit of less than 1.5 percent relative to the pylon-mounted, clean-inflow baseline. The subject research project has identified tools and methodologies necessary for the <span class="hlt">design</span> of next-generation, highly-airframe-integrated propulsion systems. These tools will be validated in future large-scale testing of the BLI inlet / fan system in NASA's 8 foot x 6 foot transonic wind tunnel. In addition, fan unsteady response to screen-generated total pressure distortion is being characterized experimentally in a JT15D engine test rig. These data will document engine sensitivities to distortion magnitude and spatial distribution, providing early insight into key physical processes that will control BLI propulsor <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=230831&keyword=ratio+AND+control&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50','EPA-EIMS'); return false;" href="https://cfpub.epa.gov/si/si_public_record_report.cfm?dirEntryId=230831&keyword=ratio+AND+control&actType=&TIMSType=+&TIMSSubTypeID=&DEID=&epaNumber=&ntisID=&archiveStatus=Both&ombCat=Any&dateBeginCreated=&dateEndCreated=&dateBeginPublishedPresented=&dateEndPublishedPresented=&dateBeginUpdated=&dateEndUpdated=&dateBeginCompleted=&dateEndCompleted=&personID=&role=Any&journalID=&publisherID=&sortBy=revisionDate&count=50"><span>Determining a <span class="hlt">Robust</span> D-Optimal <span class="hlt">Design</span> for Testing for Departure from Additivity in a Mixture of Four Perfluoroalkyl Acids.</span></a></p> <p><a target="_blank" href="http://oaspub.epa.gov/eims/query.page">EPA Science Inventory</a></p> <p></p> <p></p> <p>Our objective is to determine an optimal experimental <span class="hlt">design</span> for a mixture of perfluoroalkyl acids (PFAAs) that is <span class="hlt">robust</span> to the assumption of additivity. PFAAs are widely used in consumer products and industrial applications. The presence and persistence of PFAAs, especially in ...</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900013708','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900013708"><span>Modern CACSD using the <span class="hlt">Robust</span>-Control Toolbox</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chiang, Richard Y.; Safonov, Michael G.</p> <p>1989-01-01</p> <p>The <span class="hlt">Robust</span>-Control Toolbox is a collection of 40 M-files which extend the capability of PC/PRO-MATLAB to do modern multivariable <span class="hlt">robust</span> control system <span class="hlt">design</span>. Included are <span class="hlt">robust</span> analysis tools like singular values and structured singular values, <span class="hlt">robust</span> synthesis tools like continuous/discrete H(exp 2)/H infinity synthesis and Linear Quadratic Gaussian Loop Transfer Recovery methods and a variety of <span class="hlt">robust</span> model reduction tools such as Hankel approximation, balanced truncation and balanced stochastic truncation, etc. The capabilities of the toolbox are described and illustated with examples to show how easily they can be used in practice. Examples include structured singular value analysis, H infinity loop-shaping and large space structure model reduction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860007016','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860007016"><span><span class="hlt">Robust</span> detection-isolation-accommodation for sensor failures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Weiss, J. L.; Pattipati, K. R.; Willsky, A. S.; Eterno, J. S.; Crawford, J. T.</p> <p>1985-01-01</p> <p>The results of a one year study to: (1) develop a theory for <span class="hlt">Robust</span> Failure Detection and Identification (FDI) in the presence of model uncertainty, (2) develop a <span class="hlt">design</span> methodology which utilizes the <span class="hlt">robust</span> FDI ththeory, (3) apply the methodology to a sensor FDI problem for the F-100 jet engine, and (4) demonstrate the application of the theory to the evaluation of alternative FDI schemes are presented. Theoretical results in statistical discrimination are used to evaluate the <span class="hlt">robustness</span> of residual signals (or parity relations) in terms of their usefulness for FDI. Furthermore, optimally <span class="hlt">robust</span> parity relations are derived through the optimization of <span class="hlt">robustness</span> metrics. The result is viewed as decentralization of the FDI process. A general structure for decentralized FDI is proposed and <span class="hlt">robustness</span> metrics are used for determining various parameters of the algorithm.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930004191','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930004191"><span>Weight optimization of an aerobrake structural concept for a lunar transfer vehicle</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bush, Lance B.; Unal, Resit; Rowell, Lawrence F.; Rehder, John J.</p> <p>1992-01-01</p> <p>An aerobrake structural concept for a lunar transfer vehicle was weight optimized through the use of the <span class="hlt">Taguchi</span> <span class="hlt">design</span> method, finite element analyses, and element sizing routines. Six <span class="hlt">design</span> parameters were chosen to represent the aerobrake structural configuration. The <span class="hlt">design</span> parameters included honeycomb core thickness, diameter-depth ratio, shape, material, number of concentric ring frames, and number of radial frames. Each parameter was assigned three levels. The aerobrake structural configuration with the minimum weight was 44 percent less than the average weight of all the remaining satisfactory experimental configurations. In addition, the results of this study have served to bolster the advocacy of the <span class="hlt">Taguchi</span> method for aerospace vehicle <span class="hlt">design</span>. Both reduced analysis time and an optimized <span class="hlt">design</span> demonstrated the applicability of the <span class="hlt">Taguchi</span> method to aerospace vehicle <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920015004','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920015004"><span>Preliminary structural <span class="hlt">design</span> of a lunar transfer vehicle aerobrake. M.S. Thesis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bush, Lance B.</p> <p>1992-01-01</p> <p>An aerobrake concept for a Lunar transfer vehicle was weight optimized through the use of the <span class="hlt">Taguchi</span> <span class="hlt">design</span> method, structural finite element analyses and structural sizing routines. Six <span class="hlt">design</span> parameters were chosen to represent the aerobrake structural configuration. The <span class="hlt">design</span> parameters included honeycomb core thickness, diameter to depth ratio, shape, material, number of concentric ring frames, and number of radial frames. Each parameter was assigned three levels. The minimum weight aerobrake configuration resulting from the study was approx. half the weight of the average of all twenty seven experimental configurations. The parameters having the most significant impact on the aerobrake structural weight were identified.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014IJSyS..45.2242L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014IJSyS..45.2242L"><span><span class="hlt">Robust</span> output tracking control of a laboratory helicopter for automatic landing</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Hao; Lu, Geng; Zhong, Yisheng</p> <p>2014-11-01</p> <p>In this paper, <span class="hlt">robust</span> output tracking control problem of a laboratory helicopter for automatic landing in high seas is investigated. The motion of the helicopter is required to synchronise with that of an oscillating platform, e.g. the deck of a vessel subject to wave-induced motions. A <span class="hlt">robust</span> linear time-invariant output feedback controller consisting of a nominal controller and a <span class="hlt">robust</span> compensator is <span class="hlt">designed</span>. The <span class="hlt">robust</span> compensator is introduced to restrain the influences of parametric uncertainties, nonlinearities and external disturbances. It is shown that <span class="hlt">robust</span> stability and <span class="hlt">robust</span> tracking property can be achieved simultaneously. Experimental results on the laboratory helicopter for automatic landing demonstrate the effectiveness of the <span class="hlt">designed</span> control approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17945977','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17945977"><span><span class="hlt">Robust</span> blood-glucose control using Mathematica.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kovács, Levente; Paláncz, Béla; Benyó, Balázs; Török, László; Benyó, Zoltán</p> <p>2006-01-01</p> <p>A <span class="hlt">robust</span> control <span class="hlt">design</span> on frequency domain using Mathematica is presented for regularization of glucose level in type I diabetes persons under intensive care. The method originally proposed under Mathematica by Helton and Merino, --now with an improved disturbance rejection constraint inequality--is employed, using a three-state minimal patient model. The <span class="hlt">robustness</span> of the resulted high-order linear controller is demonstrated by nonlinear closed loop simulation in state-space, in case of standard meal disturbances and is compared with H infinity <span class="hlt">design</span> implemented with the mu-toolbox of Matlab. The controller <span class="hlt">designed</span> with model parameters represented the most favorable plant dynamics from the point of view of control purposes, can operate properly even in case of parameter values of the worst-case scenario.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010000881','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010000881"><span>Synthesis Methods for <span class="hlt">Robust</span> Passification and Control</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kelkar, Atul G.; Joshi, Suresh M. (Technical Monitor)</p> <p>2000-01-01</p> <p>The research effort under this cooperative agreement has been essentially the continuation of the work from previous grants. The ongoing work has primarily focused on developing passivity-based control techniques for Linear Time-Invariant (LTI) systems. During this period, there has been a significant progress made in the area of passivity-based control of LTI systems and some preliminary results have also been obtained for nonlinear systems, as well. The prior work has addressed optimal control <span class="hlt">design</span> for inherently passive as well as non- passive linear systems. For exploiting the <span class="hlt">robustness</span> characteristics of passivity-based controllers the passification methodology was developed for LTI systems that are not inherently passive. Various methods of passification were first proposed in and further developed. The <span class="hlt">robustness</span> of passification was addressed for multi-input multi-output (MIMO) systems for certain classes of uncertainties using frequency-domain methods. For MIMO systems, a state-space approach using Linear Matrix Inequality (LMI)-based formulation was presented, for passification of non-passive LTI systems. An LMI-based <span class="hlt">robust</span> passification technique was presented for systems with redundant actuators and sensors. The redundancy in actuators and sensors was used effectively for <span class="hlt">robust</span> passification using the LMI formulation. The passification was <span class="hlt">designed</span> to be <span class="hlt">robust</span> to an interval-type uncertainties in system parameters. The passification techniques were used to <span class="hlt">design</span> a <span class="hlt">robust</span> controller for Benchmark Active Control Technology wing under parametric uncertainties. The results on passive nonlinear systems, however, are very limited to date. Our recent work in this area was presented, wherein some stability results were obtained for passive nonlinear systems that are affine in control.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_19 --> <div id="page_20" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="381"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJC....91..937H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJC....91..937H"><span>Optimal <span class="hlt">design</span> for <span class="hlt">robust</span> control of uncertain flexible joint manipulators: a fuzzy dynamical system approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Han, Jiang; Chen, Ye-Hwa; Zhao, Xiaomin; Dong, Fangfang</p> <p>2018-04-01</p> <p>A novel fuzzy dynamical system approach to the control <span class="hlt">design</span> of flexible joint manipulators with mismatched uncertainty is proposed. Uncertainties of the system are assumed to lie within prescribed fuzzy sets. The desired system performance includes a deterministic phase and a fuzzy phase. First, by creatively implanting a fictitious control, a <span class="hlt">robust</span> control scheme is constructed to render the system uniformly bounded and uniformly ultimately bounded. Both the manipulator modelling and control scheme are deterministic and not IF-THEN heuristic rules-based. Next, a fuzzy-based performance index is proposed. An optimal <span class="hlt">design</span> problem for a control <span class="hlt">design</span> parameter is formulated as a constrained optimisation problem. The global solution to this problem can be obtained from solving two quartic equations. The fuzzy dynamical system approach is systematic and is able to assure the deterministic performance as well as to minimise the fuzzy performance index.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28587105','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28587105"><span>Internal Model-Based <span class="hlt">Robust</span> Tracking Control <span class="hlt">Design</span> for the MEMS Electromagnetic Micromirror.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tan, Jiazheng; Sun, Weijie; Yeow, John T W</p> <p>2017-05-26</p> <p>The micromirror based on micro-electro-mechanical systems (MEMS) technology is widely employed in different areas, such as scanning, imaging and optical switching. This paper studies the MEMS electromagnetic micromirror for scanning or imaging application. In these application scenarios, the micromirror is required to track the command sinusoidal signal, which can be converted to an output regulation problem theoretically. In this paper, based on the internal model principle, the output regulation problem is solved by <span class="hlt">designing</span> a <span class="hlt">robust</span> controller that is able to force the micromirror to track the command signal accurately. The proposed controller relies little on the accuracy of the model. Further, the proposed controller is implemented, and its effectiveness is examined by experiments. The experimental results demonstrate that the performance of the proposed controller is satisfying.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5492107','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5492107"><span>Internal Model-Based <span class="hlt">Robust</span> Tracking Control <span class="hlt">Design</span> for the MEMS Electromagnetic Micromirror</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Tan, Jiazheng; Sun, Weijie; Yeow, John T. W.</p> <p>2017-01-01</p> <p>The micromirror based on micro-electro-mechanical systems (MEMS) technology is widely employed in different areas, such as scanning, imaging and optical switching. This paper studies the MEMS electromagnetic micromirror for scanning or imaging application. In these application scenarios, the micromirror is required to track the command sinusoidal signal, which can be converted to an output regulation problem theoretically. In this paper, based on the internal model principle, the output regulation problem is solved by <span class="hlt">designing</span> a <span class="hlt">robust</span> controller that is able to force the micromirror to track the command signal accurately. The proposed controller relies little on the accuracy of the model. Further, the proposed controller is implemented, and its effectiveness is examined by experiments. The experimental results demonstrate that the performance of the proposed controller is satisfying. PMID:28587105</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JPS...273..413V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JPS...273..413V"><span>New charging strategy for lithium-ion batteries based on the integration of <span class="hlt">Taguchi</span> method and state of charge estimation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vo, Thanh Tu; Chen, Xiaopeng; Shen, Weixiang; Kapoor, Ajay</p> <p>2015-01-01</p> <p>In this paper, a new charging strategy of lithium-polymer batteries (LiPBs) has been proposed based on the integration of <span class="hlt">Taguchi</span> method (TM) and state of charge estimation. The TM is applied to search an optimal charging current pattern. An adaptive switching gain sliding mode observer (ASGSMO) is adopted to estimate the SOC which controls and terminates the charging process. The experimental results demonstrate that the proposed charging strategy can successfully charge the same types of LiPBs with different capacities and cycle life. The proposed charging strategy also provides much shorter charging time, narrower temperature variation and slightly higher energy efficiency than the equivalent constant current constant voltage charging method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20010039415','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20010039415"><span>Approach for Uncertainty Propagation and <span class="hlt">Robust</span> <span class="hlt">Design</span> in CFD Using Sensitivity Derivatives</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Putko, Michele M.; Newman, Perry A.; Taylor, Arthur C., III; Green, Lawrence L.</p> <p>2001-01-01</p> <p>This paper presents an implementation of the approximate statistical moment method for uncertainty propagation and <span class="hlt">robust</span> optimization for a quasi 1-D Euler CFD (computational fluid dynamics) code. Given uncertainties in statistically independent, random, normally distributed input variables, a first- and second-order statistical moment matching procedure is performed to approximate the uncertainty in the CFD output. Efficient calculation of both first- and second-order sensitivity derivatives is required. In order to assess the validity of the approximations, the moments are compared with statistical moments generated through Monte Carlo simulations. The uncertainties in the CFD input variables are also incorporated into a <span class="hlt">robust</span> optimization procedure. For this optimization, statistical moments involving first-order sensitivity derivatives appear in the objective function and system constraints. Second-order sensitivity derivatives are used in a gradient-based search to successfully execute a <span class="hlt">robust</span> optimization. The approximate methods used throughout the analyses are found to be valid when considering <span class="hlt">robustness</span> about input parameter mean values.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=Health+AND+insurance+AND+selection&id=EJ765850','ERIC'); return false;" href="https://eric.ed.gov/?q=Health+AND+insurance+AND+selection&id=EJ765850"><span>A "Politically <span class="hlt">Robust</span>" Experimental <span class="hlt">Design</span> for Public Policy Evaluation, with Application to the Mexican Universal Health Insurance Program</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>King, Gary; Gakidou, Emmanuela; Ravishankar, Nirmala; Moore, Ryan T.; Lakin, Jason; Vargas, Manett; Tellez-Rojo, Martha Maria; Avila, Juan Eugenio Hernandez; Avila, Mauricio Hernandez; Llamas, Hector Hernandez</p> <p>2007-01-01</p> <p>We develop an approach to conducting large-scale randomized public policy experiments intended to be more <span class="hlt">robust</span> to the political interventions that have ruined some or all parts of many similar previous efforts. Our proposed <span class="hlt">design</span> is insulated from selection bias in some circumstances even if we lose observations; our inferences can still be…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JMEP...26.3901G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JMEP...26.3901G"><span>Furnace Brazing Parameters Optimized by <span class="hlt">Taguchi</span> Method and Corrosion Behavior of Tube-Fin System of Automotive Condensers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Guía-Tello, J. C.; Pech-Canul, M. A.; Trujillo-Vázquez, E.; Pech-Canul, M. I.</p> <p>2017-08-01</p> <p>Controlled atmosphere brazing has a widespread industrial use in the production of aluminum automotive heat exchangers. Good-quality joints between the components depend on the initial condition of materials as well as on the brazing process parameters. In this work, the <span class="hlt">Taguchi</span> method was used to optimize the brazing parameters with respect to corrosion performance for tube-fin mini-assemblies of an automotive condenser. The experimental <span class="hlt">design</span> consisted of five factors (micro-channel tube type, flux type, peak temperature, heating rate and dwell time), with two levels each. The corrosion behavior in acidified seawater solution pH 2.8 was evaluated through potentiodynamic polarization and electrochemical impedance spectroscopy (EIS) measurements. Scanning electron microscope (SEM) and energy-dispersive x-ray spectroscopy (EDS) were used to analyze the microstructural features in the joint zone. The results showed that the parameters that most significantly affect the corrosion rate are the type of flux and the peak temperature. The optimal conditions were: micro-channel tube with 4.2 g/m2 of zinc coating, standard flux, 610 °C peak temperature, 5 °C/min heating rate and 4 min dwell time. The corrosion current density value of the confirmation experiment is in excellent agreement with the predicted value. The electrochemical characterization for selected samples gave indication that the brazing conditions had a more significant effect on the kinetics of the hydrogen evolution reaction than on the kinetics of the metal dissolution reaction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27343435','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27343435"><span>Effect of olive mill waste addition on the properties of porous fired clay bricks using <span class="hlt">Taguchi</span> method.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sutcu, Mucahit; Ozturk, Savas; Yalamac, Emre; Gencel, Osman</p> <p>2016-10-01</p> <p>Production of porous clay bricks lightened by adding olive mill waste as a pore making additive was investigated. Factors influencing the brick manufacturing process were analyzed by an experimental <span class="hlt">design</span>, <span class="hlt">Taguchi</span> method, to find out the most favorable conditions for the production of bricks. The optimum process conditions for brick preparation were investigated by studying the effects of mixture ratios (0, 5 and 10 wt%) and firing temperatures (850, 950 and 1050 °C) on the physical, thermal and mechanical properties of the bricks. Apparent density, bulk density, apparent porosity, water absorption, compressive strength, thermal conductivity, microstructure and crystalline phase formations of the fired brick samples were measured. It was found that the use of 10% waste addition reduced the bulk density of the samples up to 1.45 g/cm(3). As the porosities increased from 30.8 to 47.0%, the compressive strengths decreased from 36.9 to 10.26 MPa at firing temperature of 950 °C. The thermal conductivities of samples fired at the same temperature showed a decrease of 31% from 0.638 to 0.436 W/mK, which is hopeful for heat insulation in the buildings. Increasing of the firing temperature also affected their mechanical and physical properties. This study showed that the olive mill waste could be used as a pore maker in brick production. Copyright © 2016 Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008JLVEn..32..241M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008JLVEn..32..241M"><span>The Concept of Fashion <span class="hlt">Design</span> on the Basis of Color Coordination Using White LED Lighting</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mizutani, Yumiko; Taguchi, Tsunemasa</p> <p></p> <p>This thesis focuses on the development of fashion <span class="hlt">design</span>, especially a dress coordinated with White LED Lighting (=LED). As for the <span class="hlt">design</span> concept a fusion of the advanced science and local culture was aimed for. For such a reason this development is a very experimental one. Here in particular I handled an Imperial Court dinner dress for the last Japanese First Lady, Mrs. Akie Abe who wore it at the Imperial Court dinner for the Indonesian First Couple held on November 2006 to. This dress made by Prof. T. <span class="hlt">Taguchi</span> and I open up a new field in the dress <span class="hlt">design</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20518505','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20518505"><span>Electrostatic separation for recycling waste printed circuit board: a study on external factor and a <span class="hlt">robust</span> <span class="hlt">design</span> for optimization.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hou, Shibing; Wu, Jiang; Qin, Yufei; Xu, Zhenming</p> <p>2010-07-01</p> <p>Electrostatic separation is an effective and environmentally friendly method for recycling waste printed circuit board (PCB) by several kinds of electrostatic separators. However, some notable problems have been detected in its applications and cannot be efficiently resolved by optimizing the separation process. Instead of the separator itself, these problems are mainly caused by some external factors such as the nonconductive powder (NP) and the superficial moisture of feeding granule mixture. These problems finally lead to an inefficient separation. In the present research, the impacts of these external factors were investigated and a <span class="hlt">robust</span> <span class="hlt">design</span> was built to optimize the process and to weaken the adverse impact. A most <span class="hlt">robust</span> parameter setting (25 kv, 80 rpm) was concluded from the experimental <span class="hlt">design</span>. In addition, some theoretical methods, including cyclone separation, were presented to eliminate these problems substantially. This will contribute to efficient electrostatic separation of waste PCB and make remarkable progress for industrial applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JIEIC..96...57A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JIEIC..96...57A"><span>Parameter <span class="hlt">Design</span> in Fusion Welding of AA 6061 Aluminium Alloy using Desirability Grey Relational Analysis (DGRA) Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Adalarasan, R.; Santhanakumar, M.</p> <p>2015-01-01</p> <p>In the present work, yield strength, ultimate strength and micro-hardness of the lap joints formed with Al 6061 alloy sheets by using the processes of Tungsten Inert Gas (TIG) welding and Metal Inert Gas (MIG) welding were studied for various combinations of the welding parameters. The parameters taken for study include welding current, voltage, welding speed and inert gas flow rate. <span class="hlt">Taguchi</span>'s L9 orthogonal array was used to conduct the experiments and an integrated technique of desirability grey relational analysis was disclosed for optimizing the welding parameters. The ignored <span class="hlt">robustness</span> in desirability approach is compensated by the grey relational approach to predict the optimal setting of input parameters for the TIG and MIG welding processes which were validated through the confirmation experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1406346','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1406346"><span><span class="hlt">Robust</span> Structural Analysis and <span class="hlt">Design</span> of Distributed Control Systems to Prevent Zero Dynamics Attacks</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Weerakkody, Sean; Liu, Xiaofei; Sinopoli, Bruno</p> <p></p> <p>We consider the <span class="hlt">design</span> and analysis of <span class="hlt">robust</span> distributed control systems (DCSs) to ensure the detection of integrity attacks. DCSs are often managed by independent agents and are implemented using a diverse set of sensors and controllers. However, the heterogeneous nature of DCSs along with their scale leave such systems vulnerable to adversarial behavior. To mitigate this reality, we provide tools that allow operators to prevent zero dynamics attacks when as many as p agents and sensors are corrupted. Such a <span class="hlt">design</span> ensures attack detectability in deterministic systems while removing the threat of a class of stealthy attacks in stochasticmore » systems. To achieve this goal, we use graph theory to obtain necessary and sufficient conditions for the presence of zero dynamics attacks in terms of the structural interactions between agents and sensors. We then formulate and solve optimization problems which minimize communication networks while also ensuring a resource limited adversary cannot perform a zero dynamics attacks. Polynomial time algorithms for <span class="hlt">design</span> and analysis are provided.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880067184&hterms=decentralized&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Ddecentralized','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880067184&hterms=decentralized&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3Ddecentralized"><span>Decentralized adaptive control of robot manipulators with <span class="hlt">robust</span> stabilization <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yuan, Bau-San; Book, Wayne J.</p> <p>1988-01-01</p> <p>Due to geometric nonlinearities and complex dynamics, a decentralized technique for adaptive control for multilink robot arms is attractive. Lyapunov-function theory for stability analysis provides an approach to <span class="hlt">robust</span> stabilization. Each joint of the arm is treated as a component subsystem. The adaptive controller is made locally stable with servo signals including proportional and integral gains. This results in the bound on the dynamical interactions with other subsystems. A nonlinear controller which stabilizes the system with uniform boundedness is used to improve the <span class="hlt">robustness</span> properties of the overall system. As a result, the robot tracks the reference trajectories with convergence. This strategy makes computation simple and therefore facilitates real-time implementation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016NatCo...713255E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016NatCo...713255E"><span>A network property necessary for concentration <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Eloundou-Mbebi, Jeanne M. O.; Küken, Anika; Omranian, Nooshin; Kleessen, Sabrina; Neigenfind, Jost; Basler, Georg; Nikoloski, Zoran</p> <p>2016-10-01</p> <p>Maintenance of functionality of complex cellular networks and entire organisms exposed to environmental perturbations often depends on concentration <span class="hlt">robustness</span> of the underlying components. Yet, the reasons and consequences of concentration <span class="hlt">robustness</span> in large-scale cellular networks remain largely unknown. Here, we derive a necessary condition for concentration <span class="hlt">robustness</span> based only on the structure of networks endowed with mass action kinetics. The structural condition can be used to <span class="hlt">design</span> targeted experiments to study concentration <span class="hlt">robustness</span>. We show that metabolites satisfying the necessary condition are present in metabolic networks from diverse species, suggesting prevalence of this property across kingdoms of life. We also demonstrate that our predictions about concentration <span class="hlt">robustness</span> of energy-related metabolites are in line with experimental evidence from Escherichia coli. The necessary condition is applicable to mass action biological systems of arbitrary size, and will enable understanding the implications of concentration <span class="hlt">robustness</span> in genetic engineering strategies and medical applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27759015','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27759015"><span>A network property necessary for concentration <span class="hlt">robustness</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Eloundou-Mbebi, Jeanne M O; Küken, Anika; Omranian, Nooshin; Kleessen, Sabrina; Neigenfind, Jost; Basler, Georg; Nikoloski, Zoran</p> <p>2016-10-19</p> <p>Maintenance of functionality of complex cellular networks and entire organisms exposed to environmental perturbations often depends on concentration <span class="hlt">robustness</span> of the underlying components. Yet, the reasons and consequences of concentration <span class="hlt">robustness</span> in large-scale cellular networks remain largely unknown. Here, we derive a necessary condition for concentration <span class="hlt">robustness</span> based only on the structure of networks endowed with mass action kinetics. The structural condition can be used to <span class="hlt">design</span> targeted experiments to study concentration <span class="hlt">robustness</span>. We show that metabolites satisfying the necessary condition are present in metabolic networks from diverse species, suggesting prevalence of this property across kingdoms of life. We also demonstrate that our predictions about concentration <span class="hlt">robustness</span> of energy-related metabolites are in line with experimental evidence from Escherichia coli. The necessary condition is applicable to mass action biological systems of arbitrary size, and will enable understanding the implications of concentration <span class="hlt">robustness</span> in genetic engineering strategies and medical applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19150188','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19150188"><span>Application of multi-factorial <span class="hlt">design</span> of experiments to successfully optimize immunoassays for <span class="hlt">robust</span> measurements of therapeutic proteins.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ray, Chad A; Patel, Vimal; Shih, Judy; Macaraeg, Chris; Wu, Yuling; Thway, Theingi; Ma, Mark; Lee, Jean W; Desilva, Binodh</p> <p>2009-02-20</p> <p>Developing a process that generates <span class="hlt">robust</span> immunoassays that can be used to support studies with tight timelines is a common challenge for bioanalytical laboratories. <span class="hlt">Design</span> of experiments (DOEs) is a tool that has been used by many industries for the purpose of optimizing processes. The approach is capable of identifying critical factors and their interactions with a minimal number of experiments. The challenge for implementing this tool in the bioanalytical laboratory is to develop a user-friendly approach that scientists can understand and apply. We have successfully addressed these challenges by eliminating the screening <span class="hlt">design</span>, introducing automation, and applying a simple mathematical approach for the output parameter. A modified central composite <span class="hlt">design</span> (CCD) was applied to three ligand binding assays. The intra-plate factors selected were coating, detection antibody concentration, and streptavidin-HRP concentrations. The inter-plate factors included incubation times for each step. The objective was to maximize the logS/B (S/B) of the low standard to the blank. The maximum desirable conditions were determined using JMP 7.0. To verify the validity of the predictions, the logS/B prediction was compared against the observed logS/B during pre-study validation experiments. The three assays were optimized using the multi-factorial DOE. The total error for all three methods was less than 20% which indicated method <span class="hlt">robustness</span>. DOE identified interactions in one of the methods. The model predictions for logS/B were within 25% of the observed pre-study validation values for all methods tested. The comparison between the CCD and hybrid screening <span class="hlt">design</span> yielded comparable parameter estimates. The user-friendly <span class="hlt">design</span> enables effective application of multi-factorial DOE to optimize ligand binding assays for therapeutic proteins. The approach allows for identification of interactions between factors, consistency in optimal parameter determination, and reduced method</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.esajournals.org/doi/abs/10.1890/0012-9658(1997)078%5B0563%3AETEUCR%5D2.0.CO%3B2','USGSPUBS'); return false;" href="http://www.esajournals.org/doi/abs/10.1890/0012-9658(1997)078%5B0563%3AETEUCR%5D2.0.CO%3B2"><span>Estimating temporary emigration and breeding proportions using capture-recapture data with Pollock's <span class="hlt">robust</span> <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Kendall, W.L.; Nichols, J.D.; Hines, J.E.</p> <p>1997-01-01</p> <p>Statistical inference for capture-recapture studies of open animal populations typically relies on the assumption that all emigration from the studied population is permanent. However, there are many instances in which this assumption is unlikely to be met. We define two general models for the process of temporary emigration, completely random and Markovian. We then consider effects of these two types of temporary emigration on Jolly-Seber (Seber 1982) estimators and on estimators arising from the full-likelihood approach of Kendall et al. (1995) to <span class="hlt">robust</span> <span class="hlt">design</span> data. Capture-recapture data arising from Pollock's (1982) <span class="hlt">robust</span> <span class="hlt">design</span> provide the basis for obtaining unbiased estimates of demographic parameters in the presence of temporary emigration and for estimating the probability of temporary emigration. We present a likelihood-based approach to dealing with temporary emigration that permits estimation under different models of temporary emigration and yields tests for completely random and Markovian emigration. In addition, we use the relationship between capture probability estimates based on closed and open models under completely random temporary emigration to derive three ad hoc estimators for the probability of temporary emigration, two of which should be especially useful in situations where capture probabilities are heterogeneous among individual animals. Ad hoc and full-likelihood estimators are illustrated for small mammal capture-recapture data sets. We believe that these models and estimators will be useful for testing hypotheses about the process of temporary emigration, for estimating demographic parameters in the presence of temporary emigration, and for estimating probabilities of temporary emigration. These latter estimates are frequently of ecological interest as indicators of animal movement and, in some sampling situations, as direct estimates of breeding probabilities and proportions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3286608','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3286608"><span><span class="hlt">Robust</span> EM Continual Reassessment Method in Oncology Dose Finding</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Yuan, Ying; Yin, Guosheng</p> <p>2012-01-01</p> <p>The continual reassessment method (CRM) is a commonly used dose-finding <span class="hlt">design</span> for phase I clinical trials. Practical applications of this method have been restricted by two limitations: (1) the requirement that the toxicity outcome needs to be observed shortly after the initiation of the treatment; and (2) the potential sensitivity to the prespecified toxicity probability at each dose. To overcome these limitations, we naturally treat the unobserved toxicity outcomes as missing data, and use the expectation-maximization (EM) algorithm to estimate the dose toxicity probabilities based on the incomplete data to direct dose assignment. To enhance the <span class="hlt">robustness</span> of the <span class="hlt">design</span>, we propose prespecifying multiple sets of toxicity probabilities, each set corresponding to an individual CRM model. We carry out these multiple CRMs in parallel, across which model selection and model averaging procedures are used to make more <span class="hlt">robust</span> inference. We evaluate the operating characteristics of the proposed <span class="hlt">robust</span> EM-CRM <span class="hlt">designs</span> through simulation studies and show that the proposed methods satisfactorily resolve both limitations of the CRM. Besides improving the MTD selection percentage, the new <span class="hlt">designs</span> dramatically shorten the duration of the trial, and are <span class="hlt">robust</span> to the prespecification of the toxicity probabilities. PMID:22375092</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1408149-sequential-optimization-based-framework-robust-modeling-design-heterogeneous-catalytic-systems','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1408149-sequential-optimization-based-framework-robust-modeling-design-heterogeneous-catalytic-systems"><span>Sequential-Optimization-Based Framework for <span class="hlt">Robust</span> Modeling and <span class="hlt">Design</span> of Heterogeneous Catalytic Systems</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Rangarajan, Srinivas; Maravelias, Christos T.; Mavrikakis, Manos</p> <p>2017-11-09</p> <p>Here, we present a general optimization-based framework for (i) ab initio and experimental data driven mechanistic modeling and (ii) optimal catalyst <span class="hlt">design</span> of heterogeneous catalytic systems. Both cases are formulated as a nonlinear optimization problem that is subject to a mean-field microkinetic model and thermodynamic consistency requirements as constraints, for which we seek sparse solutions through a ridge (L 2 regularization) penalty. The solution procedure involves an iterative sequence of forward simulation of the differential algebraic equations pertaining to the microkinetic model using a numerical tool capable of handling stiff systems, sensitivity calculations using linear algebra, and gradient-based nonlinear optimization.more » A multistart approach is used to explore the solution space, and a hierarchical clustering procedure is implemented for statistically classifying potentially competing solutions. An example of methanol synthesis through hydrogenation of CO and CO 2 on a Cu-based catalyst is used to illustrate the framework. The framework is fast, is <span class="hlt">robust</span>, and can be used to comprehensively explore the model solution and <span class="hlt">design</span> space of any heterogeneous catalytic system.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1408149-sequential-optimization-based-framework-robust-modeling-design-heterogeneous-catalytic-systems','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1408149-sequential-optimization-based-framework-robust-modeling-design-heterogeneous-catalytic-systems"><span>Sequential-Optimization-Based Framework for <span class="hlt">Robust</span> Modeling and <span class="hlt">Design</span> of Heterogeneous Catalytic Systems</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Rangarajan, Srinivas; Maravelias, Christos T.; Mavrikakis, Manos</p> <p></p> <p>Here, we present a general optimization-based framework for (i) ab initio and experimental data driven mechanistic modeling and (ii) optimal catalyst <span class="hlt">design</span> of heterogeneous catalytic systems. Both cases are formulated as a nonlinear optimization problem that is subject to a mean-field microkinetic model and thermodynamic consistency requirements as constraints, for which we seek sparse solutions through a ridge (L 2 regularization) penalty. The solution procedure involves an iterative sequence of forward simulation of the differential algebraic equations pertaining to the microkinetic model using a numerical tool capable of handling stiff systems, sensitivity calculations using linear algebra, and gradient-based nonlinear optimization.more » A multistart approach is used to explore the solution space, and a hierarchical clustering procedure is implemented for statistically classifying potentially competing solutions. An example of methanol synthesis through hydrogenation of CO and CO 2 on a Cu-based catalyst is used to illustrate the framework. The framework is fast, is <span class="hlt">robust</span>, and can be used to comprehensively explore the model solution and <span class="hlt">design</span> space of any heterogeneous catalytic system.« less</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_20 --> <div id="page_21" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="401"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27721510','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27721510"><span>β-galactosidase Production by Aspergillus niger ATCC 9142 Using Inexpensive Substrates in Solid-State Fermentation: Optimization by Orthogonal Arrays <span class="hlt">Design</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kazemi, Samaneh; Khayati, Gholam; Faezi-Ghasemi, Mohammad</p> <p>2016-01-01</p> <p>Enzymatic hydrolysis of lactose is one of the most important biotechnological processes in the food industry, which is accomplished by enzyme β-galactosidase (β-gal, β-D-galactoside galactohydrolase, EC 3.2.1.23), trivial called lactase. Orthogonal arrays <span class="hlt">design</span> is an appropriate option for the optimization of biotechnological processes for the production of microbial enzymes. <span class="hlt">Design</span> of experimental (DOE) methodology using <span class="hlt">Taguchi</span> orthogonal array (OA) was employed to screen the most significant levels of parameters, including the solid substrates (wheat straw, rice straw, and peanut pod), the carbon/nitrogen (C/N) ratios, the incubation time, and the inducer. The level of β-gal production was measured by a photometric enzyme activity assay using the artificial substrate ortho-Nitrophenyl-β-D-galactopyranoside. The results showed that C/N ratio (0.2% [w/v], incubation time (144 hour), and solid substrate (wheat straw) were the best conditions determined by the <span class="hlt">design</span> of experiments using the <span class="hlt">Taguchi</span> approach. Our finding showed that the use of rice straw and peanut pod, as solid-state substrates, led to 2.041-folds increase in the production of the enzyme, as compared to rice straw. In addition, the presence of an inducer did not have any significant impact on the enzyme production levels.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030002671','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030002671"><span>Optimization of Systems with Uncertainty: Initial Developments for Performance, <span class="hlt">Robustness</span> and Reliability Based <span class="hlt">Designs</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crespo, Luis G.; Bushnell, Dennis M. (Technical Monitor)</p> <p>2002-01-01</p> <p>This paper presents a study on the optimization of systems with structured uncertainties, whose inputs and outputs can be exhaustively described in the probabilistic sense. By propagating the uncertainty from the input to the output in the space of the probability density functions and the moments, optimization problems that pursue performance, <span class="hlt">robustness</span> and reliability based <span class="hlt">designs</span> are studied. Be specifying the desired outputs in terms of desired probability density functions and then in terms of meaningful probabilistic indices, we settle a computationally viable framework for solving practical optimization problems. Applications to static optimization and stability control are used to illustrate the relevance of incorporating uncertainty in the early stages of the <span class="hlt">design</span>. Several examples that admit a full probabilistic description of the output in terms of the <span class="hlt">design</span> variables and the uncertain inputs are used to elucidate the main features of the generic problem and its solution. Extensions to problems that do not admit closed form solutions are also evaluated. Concrete evidence of the importance of using a consistent probabilistic formulation of the optimization problem and a meaningful probabilistic description of its solution is provided in the examples. In the stability control problem the analysis shows that standard deterministic approaches lead to <span class="hlt">designs</span> with high probability of running into instability. The implementation of such <span class="hlt">designs</span> can indeed have catastrophic consequences.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..310a2128K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..310a2128K"><span><span class="hlt">Design</span> and analysis of a magneto-rheological damper for an all terrain vehicle</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Krishnan Unni, R.; Tamilarasan, N.</p> <p>2018-02-01</p> <p>A shock absorber <span class="hlt">design</span> intended to replace the existing conventional shock absorber with a controllable system using a Magneto-rheological damper is introduced for an All Terrain Vehicle (ATV) that was <span class="hlt">designed</span> for Baja SAE competitions. Suspensions are a vital part of an All Terrain Vehicles as it endures various surfaces and requires utmost attention while <span class="hlt">designing</span>. COMSOL multi-physics software is used for applications that have coupled physics problems and is a unique tool that is used for the <span class="hlt">designing</span> and analysis phase of the Magneto-rheological damper for the considered application and the model is optimized based on <span class="hlt">Taguchi</span> using DOE software. The magneto-rheological damper is <span class="hlt">designed</span> to maximize the damping force with the measured geometric constraints for the All Terrain Vehicle.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5075777','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5075777"><span>A network property necessary for concentration <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Eloundou-Mbebi, Jeanne M. O.; Küken, Anika; Omranian, Nooshin; Kleessen, Sabrina; Neigenfind, Jost; Basler, Georg; Nikoloski, Zoran</p> <p>2016-01-01</p> <p>Maintenance of functionality of complex cellular networks and entire organisms exposed to environmental perturbations often depends on concentration <span class="hlt">robustness</span> of the underlying components. Yet, the reasons and consequences of concentration <span class="hlt">robustness</span> in large-scale cellular networks remain largely unknown. Here, we derive a necessary condition for concentration <span class="hlt">robustness</span> based only on the structure of networks endowed with mass action kinetics. The structural condition can be used to <span class="hlt">design</span> targeted experiments to study concentration <span class="hlt">robustness</span>. We show that metabolites satisfying the necessary condition are present in metabolic networks from diverse species, suggesting prevalence of this property across kingdoms of life. We also demonstrate that our predictions about concentration <span class="hlt">robustness</span> of energy-related metabolites are in line with experimental evidence from Escherichia coli. The necessary condition is applicable to mass action biological systems of arbitrary size, and will enable understanding the implications of concentration <span class="hlt">robustness</span> in genetic engineering strategies and medical applications. PMID:27759015</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016IJC....89.1285X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016IJC....89.1285X"><span>A new smooth <span class="hlt">robust</span> control <span class="hlt">design</span> for uncertain nonlinear systems with non-vanishing disturbances</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xian, Bin; Zhang, Yao</p> <p>2016-06-01</p> <p>In this paper, we consider the control problem for a general class of nonlinear system subjected to uncertain dynamics and non-varnishing disturbances. A smooth nonlinear control algorithm is presented to tackle these uncertainties and disturbances. The proposed control <span class="hlt">design</span> employs the integral of a nonlinear sigmoid function to compensate the uncertain dynamics, and achieve a uniformly semi-global practical asymptotic stable tracking control of the system outputs. A novel Lyapunov-based stability analysis is employed to prove the convergence of the tracking errors and the stability of the closed-loop system. Numerical simulation results on a two-link robot manipulator are presented to illustrate the performance of the proposed control algorithm comparing with the layer-boundary sliding mode controller and the <span class="hlt">robust</span> of integration of sign of error control <span class="hlt">design</span>. Furthermore, real-time experiment results for the attitude control of a quadrotor helicopter are also included to confirm the effectiveness of the proposed algorithm.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890065237&hterms=dynamical+system&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Ddynamical%2Bsystem','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890065237&hterms=dynamical+system&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Ddynamical%2Bsystem"><span><span class="hlt">Robust</span> control synthesis for uncertain dynamical systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Byun, Kuk-Whan; Wie, Bong; Sunkel, John</p> <p>1989-01-01</p> <p>This paper presents <span class="hlt">robust</span> control synthesis techniques for uncertain dynamical systems subject to structured parameter perturbation. Both QFT (quantitative feedback theory) and H-infinity control synthesis techniques are investigated. Although most H-infinity-related control techniques are not concerned with the structured parameter perturbation, a new way of incorporating the parameter uncertainty in the <span class="hlt">robust</span> H-infinity control <span class="hlt">design</span> is presented. A generic model of uncertain dynamical systems is used to illustrate the <span class="hlt">design</span> methodologies investigated in this paper. It is shown that, for a certain noncolocated structural control problem, use of both techniques results in nonminimum phase compensation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005AIPC..778..145Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005AIPC..778..145Z"><span>Visualization of the Invisible, Explanation of the Unknown, Ruggedization of the Unstable: Sensitivity Analysis, Virtual Tryout and <span class="hlt">Robust</span> <span class="hlt">Design</span> through Systematic Stochastic Simulation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zwickl, Titus; Carleer, Bart; Kubli, Waldemar</p> <p>2005-08-01</p> <p>In the past decade, sheet metal forming simulation became a well established tool to predict the formability of parts. In the automotive industry, this has enabled significant reduction in the cost and time for vehicle <span class="hlt">design</span> and development, and has helped to improve the quality and performance of vehicle parts. However, production stoppages for troubleshooting and unplanned die maintenance, as well as production quality fluctuations continue to plague manufacturing cost and time. The focus therefore has shifted in recent times beyond mere feasibility to <span class="hlt">robustness</span> of the product and process being engineered. Ensuring <span class="hlt">robustness</span> is the next big challenge for the virtual tryout / simulation technology. We introduce new methods, based on systematic stochastic simulations, to visualize the behavior of the part during the whole forming process — in simulation as well as in production. Sensitivity analysis explains the response of the part to changes in influencing parameters. Virtual tryout allows quick exploration of changed <span class="hlt">designs</span> and conditions. <span class="hlt">Robust</span> <span class="hlt">design</span> and manufacturing guarantees quality and process capability for the production process. While conventional simulations helped to reduce development time and cost by ensuring feasible processes, <span class="hlt">robustness</span> engineering tools have the potential for far greater cost and time savings. Through examples we illustrate how expected and unexpected behavior of deep drawing parts may be tracked down, identified and assigned to the influential parameters. With this knowledge, defects can be eliminated or springback can be compensated e.g.; the response of the part to uncontrollable noise can be predicted and minimized. The newly introduced methods enable more reliable and predictable stamping processes in general.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011AIPC.1383..978W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011AIPC.1383..978W"><span>Efficient <span class="hlt">Robust</span> Optimization of Metal Forming Processes using a Sequential Metamodel Based Strategy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wiebenga, J. H.; Klaseboer, G.; van den Boogaard, A. H.</p> <p>2011-08-01</p> <p>The coupling of Finite Element (FE) simulations to mathematical optimization techniques has contributed significantly to product improvements and cost reductions in the metal forming industries. The next challenge is to bridge the gap between deterministic optimization techniques and the industrial need for <span class="hlt">robustness</span>. This paper introduces a new and generally applicable structured methodology for modeling and solving <span class="hlt">robust</span> optimization problems. Stochastic <span class="hlt">design</span> variables or noise variables are taken into account explicitly in the optimization procedure. The metamodel-based strategy is combined with a sequential improvement algorithm to efficiently increase the accuracy of the objective function prediction. This is only done at regions of interest containing the optimal <span class="hlt">robust</span> <span class="hlt">design</span>. Application of the methodology to an industrial V-bending process resulted in valuable process insights and an improved <span class="hlt">robust</span> process <span class="hlt">design</span>. Moreover, a significant improvement of the <span class="hlt">robustness</span> (>2σ) was obtained by minimizing the deteriorating effects of several noise variables. The <span class="hlt">robust</span> optimization results demonstrate the general applicability of the <span class="hlt">robust</span> optimization strategy and underline the importance of including uncertainty and <span class="hlt">robustness</span> explicitly in the numerical optimization procedure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596974','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596974"><span>A Unifying Mathematical Framework for Genetic <span class="hlt">Robustness</span>, Environmental <span class="hlt">Robustness</span>, Network <span class="hlt">Robustness</span> and their Tradeoff on Phenotype <span class="hlt">Robustness</span> in Biological Networks Part II: Ecological Networks</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chen, Bor-Sen; Lin, Ying-Po</p> <p>2013-01-01</p> <p>In ecological networks, network <span class="hlt">robustness</span> should be large enough to confer intrinsic <span class="hlt">robustness</span> for tolerating intrinsic parameter fluctuations, as well as environmental <span class="hlt">robustness</span> for resisting environmental disturbances, so that the phenotype stability of ecological networks can be maintained, thus guaranteeing phenotype <span class="hlt">robustness</span>. However, it is difficult to analyze the network <span class="hlt">robustness</span> of ecological systems because they are complex nonlinear partial differential stochastic systems. This paper develops a unifying mathematical framework for investigating the principles of both <span class="hlt">robust</span> stabilization and environmental disturbance sensitivity in ecological networks. We found that the phenotype <span class="hlt">robustness</span> criterion for ecological networks is that if intrinsic <span class="hlt">robustness</span> + environmental <span class="hlt">robustness</span> ≦ network <span class="hlt">robustness</span>, then the phenotype <span class="hlt">robustness</span> can be maintained in spite of intrinsic parameter fluctuations and environmental disturbances. These results in <span class="hlt">robust</span> ecological networks are similar to that in <span class="hlt">robust</span> gene regulatory networks and evolutionary networks even they have different spatial-time scales. PMID:23515112</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18971928','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18971928"><span>A fast, <span class="hlt">robust</span> and tunable synthetic gene oscillator.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Stricker, Jesse; Cookson, Scott; Bennett, Matthew R; Mather, William H; Tsimring, Lev S; Hasty, Jeff</p> <p>2008-11-27</p> <p>One defining goal of synthetic biology is the development of engineering-based approaches that enable the construction of gene-regulatory networks according to '<span class="hlt">design</span> specifications' generated from computational modelling. This approach provides a systematic framework for exploring how a given regulatory network generates a particular phenotypic behaviour. Several fundamental gene circuits have been developed using this approach, including toggle switches and oscillators, and these have been applied in new contexts such as triggered biofilm development and cellular population control. Here we describe an engineered genetic oscillator in Escherichia coli that is fast, <span class="hlt">robust</span> and persistent, with tunable oscillatory periods as fast as 13 min. The oscillator was <span class="hlt">designed</span> using a previously modelled network architecture comprising linked positive and negative feedback loops. Using a microfluidic platform tailored for single-cell microscopy, we precisely control environmental conditions and monitor oscillations in individual cells through multiple cycles. Experiments reveal remarkable <span class="hlt">robustness</span> and persistence of oscillations in the <span class="hlt">designed</span> circuit; almost every cell exhibited large-amplitude fluorescence oscillations throughout observation runs. The oscillatory period can be tuned by altering inducer levels, temperature and the media source. Computational modelling demonstrates that the key <span class="hlt">design</span> principle for constructing a <span class="hlt">robust</span> oscillator is a time delay in the negative feedback loop, which can mechanistically arise from the cascade of cellular processes involved in forming a functional transcription factor. The positive feedback loop increases the <span class="hlt">robustness</span> of the oscillations and allows for greater tunability. Examination of our refined model suggested the existence of a simplified oscillator <span class="hlt">design</span> without positive feedback, and we construct an oscillator strain confirming this computational prediction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1991NIMPA.304..364J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1991NIMPA.304..364J"><span><span class="hlt">Robust</span> control of accelerators</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Joel, W.; Johnson, D.; Chaouki, Abdallah T.</p> <p>1991-07-01</p> <p>The problem of controlling the variations in the rf power system can be effectively cast as an application of modern control theory. Two components of this theory are obtaining a model and a feedback structure. The model inaccuracies influence the choice of a particular controller structure. Because of the modelling uncertainty, one has to <span class="hlt">design</span> either a variable, adaptive controller or a fixed, <span class="hlt">robust</span> controller to achieve the desired objective. The adaptive control scheme usually results in very complex hardware; and, therefore, shall not be pursued in this research. In contrast, the <span class="hlt">robust</span> control method leads to simpler hardware. However, <span class="hlt">robust</span> control requires a more accurate mathematical model of the physical process than is required by adaptive control. Our research at the Los Alamos National Laboratory (LANL) and the University of New Mexico (UNM) has led to the development and implementation of a new <span class="hlt">robust</span> rf power feedback system. In this article, we report on our research progress. In section 1, the <span class="hlt">robust</span> control problem for the rf power system and the philosophy adopted for the beginning phase of our research is presented. In section 2, the results of our proof-of-principle experiments are presented. In section 3, we describe the actual controller configuration that is used in LANL FEL physics experiments. The novelty of our approach is that the control hardware is implemented directly in rf. without demodulating, compensating, and then remodulating.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MS%26E..184a2048H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MS%26E..184a2048H"><span>Flank wear analysing of high speed end milling for hardened steel D2 using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hazza Faizi Al-Hazza, Muataz; Ibrahim, Nur Asmawiyah bt; Adesta, Erry T. Y.; Khan, Ahsan Ali; Abdullah Sidek, Atiah Bt.</p> <p>2017-03-01</p> <p>One of the main challenges for any manufacturer is how to decrease the machining cost without affecting the final quality of the product. One of the new advanced machining processes in industry is the high speed hard end milling process that merges three advanced machining processes: high speed milling, hard milling and dry milling. However, one of the most important challenges in this process is to control the flank wear rate. Therefore a analyzing the flank wear rate during machining should be investigated in order to determine the best cutting levels that will not affect the final quality of the product. In this research <span class="hlt">Taguchi</span> method has been used to investigate the effect of cutting speed, feed rate and depth of cut and determine the best level s to minimize the flank wear rate up to total length of 0.3mm based on the ISO standard to maintain the finishing requirements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930010273','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930010273"><span>Nonlinear <span class="hlt">robust</span> controller <span class="hlt">design</span> for multi-robot systems with unknown payloads</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Song, Y. D.; Anderson, J. N.; Homaifar, A.; Lai, H. Y.</p> <p>1992-01-01</p> <p>This work is concerned with the control problem of a multi-robot system handling a payload with unknown mass properties. Force constraints at the grasp points are considered. <span class="hlt">Robust</span> control schemes are proposed that cope with the model uncertainty and achieve asymptotic path tracking. To deal with the force constraints, a strategy for optimally sharing the task is suggested. This strategy basically consists of two steps. The first detects the robots that need help and the second arranges that help. It is shown that the overall system is not only <span class="hlt">robust</span> to uncertain payload parameters, but also satisfies the force constraints.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JNEng..12d6004W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JNEng..12d6004W"><span><span class="hlt">Robust</span> control of burst suppression for medical coma</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Westover, M. Brandon; Kim, Seong-Eun; Ching, ShiNung; Purdon, Patrick L.; Brown, Emery N.</p> <p>2015-08-01</p> <p>Objective. Medical coma is an anesthetic-induced state of brain inactivation, manifest in the electroencephalogram by burst suppression. Feedback control can be used to regulate burst suppression, however, previous <span class="hlt">designs</span> have not been <span class="hlt">robust</span>. <span class="hlt">Robust</span> control <span class="hlt">design</span> is critical under real-world operating conditions, subject to substantial pharmacokinetic and pharmacodynamic parameter uncertainty and unpredictable external disturbances. We sought to develop a <span class="hlt">robust</span> closed-loop anesthesia delivery (CLAD) system to control medical coma. Approach. We developed a <span class="hlt">robust</span> CLAD system to control the burst suppression probability (BSP). We developed a novel BSP tracking algorithm based on realistic models of propofol pharmacokinetics and pharmacodynamics. We also developed a practical method for estimating patient-specific pharmacodynamics parameters. Finally, we synthesized a <span class="hlt">robust</span> proportional integral controller. Using a factorial <span class="hlt">design</span> spanning patient age, mass, height, and gender, we tested whether the system performed within clinically acceptable limits. Throughout all experiments we subjected the system to disturbances, simulating treatment of refractory status epilepticus in a real-world intensive care unit environment. Main results. In 5400 simulations, CLAD behavior remained within specifications. Transient behavior after a step in target BSP from 0.2 to 0.8 exhibited a rise time (the median (min, max)) of 1.4 [1.1, 1.9] min; settling time, 7.8 [4.2, 9.0] min; and percent overshoot of 9.6 [2.3, 10.8]%. Under steady state conditions the CLAD system exhibited a median error of 0.1 [-0.5, 0.9]%; inaccuracy of 1.8 [0.9, 3.4]%; oscillation index of 1.8 [0.9, 3.4]%; and maximum instantaneous propofol dose of 4.3 [2.1, 10.5] mg kg-1. The maximum hourly propofol dose was 4.3 [2.1, 10.3] mg kg-1 h-1. Performance fell within clinically acceptable limits for all measures. Significance. A CLAD system <span class="hlt">designed</span> using <span class="hlt">robust</span> control theory achieves clinically acceptable</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4517835','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4517835"><span><span class="hlt">Robust</span> control of burst suppression for medical coma</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Westover, M Brandon; Kim, Seong-Eun; Ching, ShiNung; Purdon, Patrick L; Brown, Emery N</p> <p>2015-01-01</p> <p>Objective Medical coma is an anesthetic-induced state of brain inactivation, manifest in the electroencephalogram by burst suppression. Feedback control can be used to regulate burst suppression, however, previous <span class="hlt">designs</span> have not been <span class="hlt">robust</span>. <span class="hlt">Robust</span> control <span class="hlt">design</span> is critical under real-world operating conditions, subject to substantial pharmacokinetic and pharmacodynamic parameter uncertainty and unpredictable external disturbances. We sought to develop a <span class="hlt">robust</span> closed-loop anesthesia delivery (CLAD) system to control medical coma. Approach We developed a <span class="hlt">robust</span> CLAD system to control the burst suppression probability (BSP). We developed a novel BSP tracking algorithm based on realistic models of propofol pharmacokinetics and pharmacodynamics. We also developed a practical method for estimating patient-specific pharmacodynamics parameters. Finally, we synthesized a <span class="hlt">robust</span> proportional integral controller. Using a factorial <span class="hlt">design</span> spanning patient age, mass, height, and gender, we tested whether the system performed within clinically acceptable limits. Throughout all experiments we subjected the system to disturbances, simulating treatment of refractory status epilepticus in a real-world intensive care unit environment. Main results In 5400 simulations, CLAD behavior remained within specifications. Transient behavior after a step in target BSP from 0.2 to 0.8 exhibited a rise time (the median (min, max)) of 1.4 [1.1, 1.9] min; settling time, 7.8 [4.2, 9.0] min; and percent overshoot of 9.6 [2.3, 10.8]%. Under steady state conditions the CLAD system exhibited a median error of 0.1 [−0.5, 0.9]%; inaccuracy of 1.8 [0.9, 3.4]%; oscillation index of 1.8 [0.9, 3.4]%; and maximum instantaneous propofol dose of 4.3 [2.1, 10.5] mg kg−1. The maximum hourly propofol dose was 4.3 [2.1, 10.3] mg kg−1 h−1. Performance fell within clinically acceptable limits for all measures. Significance A CLAD system <span class="hlt">designed</span> using <span class="hlt">robust</span> control theory achieves clinically acceptable</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20050050943','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20050050943"><span>Approach for Input Uncertainty Propagation and <span class="hlt">Robust</span> <span class="hlt">Design</span> in CFD Using Sensitivity Derivatives</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Putko, Michele M.; Taylor, Arthur C., III; Newman, Perry A.; Green, Lawrence L.</p> <p>2002-01-01</p> <p>An implementation of the approximate statistical moment method for uncertainty propagation and <span class="hlt">robust</span> optimization for quasi 3-D Euler CFD code is presented. Given uncertainties in statistically independent, random, normally distributed input variables, first- and second-order statistical moment procedures are performed to approximate the uncertainty in the CFD output. Efficient calculation of both first- and second-order sensitivity derivatives is required. In order to assess the validity of the approximations, these moments are compared with statistical moments generated through Monte Carlo simulations. The uncertainties in the CFD input variables are also incorporated into a <span class="hlt">robust</span> optimization procedure. For this optimization, statistical moments involving first-order sensitivity derivatives appear in the objective function and system constraints. Second-order sensitivity derivatives are used in a gradient-based search to successfully execute a <span class="hlt">robust</span> optimization. The approximate methods used throughout the analyses are found to be valid when considering <span class="hlt">robustness</span> about input parameter mean values.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28675693','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28675693"><span>Application of iterative <span class="hlt">robust</span> model-based optimal experimental <span class="hlt">design</span> for the calibration of biocatalytic models.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Van Daele, Timothy; Gernaey, Krist V; Ringborg, Rolf H; Börner, Tim; Heintz, Søren; Van Hauwermeiren, Daan; Grey, Carl; Krühne, Ulrich; Adlercreutz, Patrick; Nopens, Ingmar</p> <p>2017-09-01</p> <p>The aim of model calibration is to estimate unique parameter values from available experimental data, here applied to a biocatalytic process. The traditional approach of first gathering data followed by performing a model calibration is inefficient, since the information gathered during experimentation is not actively used to optimize the experimental <span class="hlt">design</span>. By applying an iterative <span class="hlt">robust</span> model-based optimal experimental <span class="hlt">design</span>, the limited amount of data collected is used to <span class="hlt">design</span> additional informative experiments. The algorithm is used here to calibrate the initial reaction rate of an ω-transaminase catalyzed reaction in a more accurate way. The parameter confidence region estimated from the Fisher Information Matrix is compared with the likelihood confidence region, which is not only more accurate but also a computationally more expensive method. As a result, an important deviation between both approaches is found, confirming that linearization methods should be applied with care for nonlinear models. © 2017 American Institute of Chemical Engineers Biotechnol. Prog., 33:1278-1293, 2017. © 2017 American Institute of Chemical Engineers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4142162','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4142162"><span><span class="hlt">Robust</span> Fuzzy Logic Stabilization with Disturbance Elimination</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Danapalasingam, Kumeresan A.</p> <p>2014-01-01</p> <p>A <span class="hlt">robust</span> fuzzy logic controller is proposed for stabilization and disturbance rejection in nonlinear control systems of a particular type. The dynamic feedback controller is <span class="hlt">designed</span> as a combination of a control law that compensates for nonlinear terms in a control system and a dynamic fuzzy logic controller that addresses unknown model uncertainties and an unmeasured disturbance. Since it is challenging to derive a highly accurate mathematical model, the proposed controller requires only nominal functions of a control system. In this paper, a mathematical derivation is carried out to prove that the controller is able to achieve asymptotic stability by processing state measurements. <span class="hlt">Robustness</span> here refers to the ability of the controller to asymptotically steer the state vector towards the origin in the presence of model uncertainties and a disturbance input. Simulation results of the <span class="hlt">robust</span> fuzzy logic controller application in a magnetic levitation system demonstrate the feasibility of the control <span class="hlt">design</span>. PMID:25177713</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MSSP...91....1H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MSSP...91....1H"><span>An info-gap application to <span class="hlt">robust</span> <span class="hlt">design</span> of a prestressed space structure under epistemic uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hot, Aurélien; Weisser, Thomas; Cogan, Scott</p> <p>2017-07-01</p> <p>Uncertainty quantification is an integral part of the model validation process and is important to take into account during the <span class="hlt">design</span> of mechanical systems. Sources of uncertainty are diverse but generally fall into two categories: aleatory due to random process and epistemic resulting from a lack of knowledge. This work focuses on the behavior of solar arrays in their stowed configuration. To avoid impacts during launch, snubbers are used to prestress the panels. Since the mechanical properties of the snubbers and the associated preload configurations are difficult to characterize precisely, an info-gap approach is proposed to investigate the influence of such uncertainties on <span class="hlt">design</span> configurations obtained for different values of safety factors. This eventually allows to revise the typical values of these factors and to reevaluate them with respect to a targeted <span class="hlt">robustness</span> level. The proposed methodology is illustrated using a simplified finite element model of a solar array.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJC....91..359S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJC....91..359S"><span><span class="hlt">Robust</span> model predictive control for constrained continuous-time nonlinear systems</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sun, Tairen; Pan, Yongping; Zhang, Jun; Yu, Haoyong</p> <p>2018-02-01</p> <p>In this paper, a <span class="hlt">robust</span> model predictive control (MPC) is <span class="hlt">designed</span> for a class of constrained continuous-time nonlinear systems with bounded additive disturbances. The <span class="hlt">robust</span> MPC consists of a nonlinear feedback control and a continuous-time model-based dual-mode MPC. The nonlinear feedback control guarantees the actual trajectory being contained in a tube centred at the nominal trajectory. The dual-mode MPC is <span class="hlt">designed</span> to ensure asymptotic convergence of the nominal trajectory to zero. This paper extends current results on discrete-time model-based tube MPC and linear system model-based tube MPC to continuous-time nonlinear model-based tube MPC. The feasibility and <span class="hlt">robustness</span> of the proposed <span class="hlt">robust</span> MPC have been demonstrated by theoretical analysis and applications to a cart-damper springer system and a one-link robot manipulator.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_21 --> <div id="page_22" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="421"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26903773','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26903773"><span>An integrated <span class="hlt">Taguchi</span> and response surface methodological approach for the optimization of an HPLC method to determine glimepiride in a supersaturatable self-nanoemulsifying formulation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Dash, Rajendra Narayan; Mohammed, Habibuddin; Humaira, Touseef</p> <p>2016-01-01</p> <p>We studied the application of <span class="hlt">Taguchi</span> orthogonal array (TOA) <span class="hlt">design</span> during the development of an isocratic stability indicating HPLC method for glimepiride as per TOA <span class="hlt">design</span>; twenty-seven experiments were conducted by varying six chromatographic factors. Percentage of organic phase was the most significant (p < 0.001) on retention time, while buffer pH had the most significant (p < 0.001) effect on tailing factor and theoretical plates. TOA <span class="hlt">design</span> has shortcoming, which identifies the only linear effect, while ignoring the quadratic and interaction effects. Hence, a response surface model for each response was created including the linear, quadratic and interaction terms. The developed models for each response found to be well predictive bearing an acceptable adjusted correlation coefficient (0.9152 for retention time, 0.8985 for tailing factor and 0.8679 for theoretical plates). The models were found to be significant (p < 0.001) having a high F value for each response (15.76 for retention time, 13.12 for tailing factor and 9.99 for theoretical plates). The optimal chromatographic condition uses acetonitrile - potassium dihydrogen phosphate (pH 4.0; 30 mM) (50:50, v/v) as the mobile phase. The temperature, flow rate and injection volume were selected as 35 ± 2 °C, 1.0 mL min(-1) and 20 μL respectively. The method was validated as per ICH guidelines and was found to be specific for analyzing glimepiride from a novel supersaturatable self-nanoemulsifying formulation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvA..97d2324Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvA..97d2324Y"><span>Neural-network-<span class="hlt">designed</span> pulse sequences for <span class="hlt">robust</span> control of singlet-triplet qubits</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, Xu-Chen; Yung, Man-Hong; Wang, Xin</p> <p>2018-04-01</p> <p>Composite pulses are essential for universal manipulation of singlet-triplet spin qubits. In the absence of noise, they are required to perform arbitrary single-qubit operations due to the special control constraint of a singlet-triplet qubit, while in a noisy environment, more complicated sequences have been developed to dynamically correct the error. Tailoring these sequences typically requires numerically solving a set of nonlinear equations. Here we demonstrate that these pulse sequences can be generated by a well-trained, double-layer neural network. For sequences <span class="hlt">designed</span> for the noise-free case, the trained neural network is capable of producing almost exactly the same pulses known in the literature. For more complicated noise-correcting sequences, the neural network produces pulses with slightly different line shapes, but the <span class="hlt">robustness</span> against noises remains comparable. These results indicate that the neural network can be a judicious and powerful alternative to existing techniques in developing pulse sequences for universal fault-tolerant quantum computation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JIEIC..97..547K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JIEIC..97..547K"><span>Wear Evaluation of AISI 4140 Alloy Steel with WC/C Lamellar Coatings Sliding Against EN 8 Using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kadam, Nikhil Rajendra; Karthikeyan, Ganesarethinam</p> <p>2016-10-01</p> <p>The purpose of the experiments in this paper is to use the <span class="hlt">Taguchi</span> methods to investigate the wear of WC/C coated nitrided AISI 4140 alloy steel. A study of lamellar WC/C coating which were deposited by a physical vapor deposition on nitrided AISI 4140 alloy steel. The investigation includes wear evaluation using Pin-on-disk configuration. When WC/C coated AISI 4140 alloy steel slides against EN 8 steel, it was found that carbon-rich coatings show much lower wear of the countersurface than nitrogen-rich coatings. The results were correlated with the properties determined from tribological and mechanical characterization, therefore by probably selecting the proper processing parameters the deposition of WC/C coating results in decreasing the wear rate of the substrate which shows a potential for tribological application.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..342a2006A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..342a2006A"><span>Costing improvement of remanufacturing crankshaft by integrating Mahalanobis-<span class="hlt">Taguchi</span> System and Activity based Costing</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Abu, M. Y.; Nor, E. E. Mohd; Rahman, M. S. Abd</p> <p>2018-04-01</p> <p>Integration between quality and costing system is very crucial in order to achieve an accurate product cost and profit. Current practice by most of remanufacturers, there are still lacking on optimization during the remanufacturing process which contributed to incorrect variables consideration to the costing system. Meanwhile, traditional costing accounting being practice has distortion in the cost unit which lead to inaccurate cost of product. The aim of this work is to identify the critical and non-critical variables during remanufacturing process using Mahalanobis-<span class="hlt">Taguchi</span> System and simultaneously estimate the cost using Activity Based Costing method. The orthogonal array was applied to indicate the contribution of variables in the factorial effect graph and the critical variables were considered with overhead costs that are actually demanding the activities. This work improved the quality inspection together with costing system to produce an accurate profitability information. As a result, the cost per unit of remanufactured crankshaft of MAN engine model with 5 critical crankpins is MYR609.50 while Detroit engine model with 4 critical crankpins is MYR1254.80. The significant of output demonstrated through promoting green by reducing re-melting process of damaged parts to ensure consistent benefit of return cores.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPCS..110..409K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPCS..110..409K"><span>Tribological behaviour predictions of r-GO reinforced Mg composite using ANN coupled <span class="hlt">Taguchi</span> approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kavimani, V.; Prakash, K. Soorya</p> <p>2017-11-01</p> <p>This paper deals with the fabrication of reduced graphene oxide (r-GO) reinforced Magnesium Metal Matrix Composite (MMC) through a novel solvent based powder metallurgy route. Investigations over basic and functional properties of developed MMC reveals that addition of r-GO improvises the microhardness upto 64 HV but however decrement in specific wear rate is also notified. Visualization of worn out surfaces through SEM images clearly explains for the occurrence of plastic deformation and the presence of wear debris because of ploughing out action. <span class="hlt">Taguchi</span> coupled Artificial Neural Network (ANN) technique is adopted to arrive at optimal values of the input parameters such as load, reinforcement weight percentage, sliding distance and sliding velocity and thereby achieve minimal target output value viz. specific wear rate. Influence of any of the input parameter over specific wear rate studied through ANOVA reveals that load acting on pin has a major influence with 38.85% followed by r-GO wt. % of 25.82%. ANN model developed to predict specific wear rate value based on the variation of input parameter facilitates better predictability with R-value of 98.4% when compared with the outcomes of regression model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007OptLT..39..786L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007OptLT..39..786L"><span>Study of optimal laser parameters for cutting QFN packages by <span class="hlt">Taguchi</span>'s matrix method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Chen-Hao; Tsai, Ming-Jong; Yang, Ciann-Dong</p> <p>2007-06-01</p> <p>This paper reports the study of optimal laser parameters for cutting QFN (Quad Flat No-lead) packages by using a diode pumped solid-state laser system (DPSSL). The QFN cutting path includes two different materials, which are the encapsulated epoxy and a copper lead frame substrate. The <span class="hlt">Taguchi</span>'s experimental method with orthogonal array of L 9(3 4) is employed to obtain optimal combinatorial parameters. A quantified mechanism was proposed for examining the laser cutting quality of a QFN package. The influences of the various factors such as laser current, laser frequency, and cutting speed on the laser cutting quality is also examined. From the experimental results, the factors on the cutting quality in the order of decreasing significance are found to be (a) laser frequency, (b) cutting speed, and (c) laser driving current. The optimal parameters were obtained at the laser frequency of 2 kHz, the cutting speed of 2 mm/s, and the driving current of 29 A. Besides identifying this sequence of dominance, matrix experiment also determines the best level for each control factor. The verification experiment confirms that the application of laser cutting technology to QFN is very successfully by using the optimal laser parameters predicted from matrix experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19900060623&hterms=feedforward+control&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dfeedforward%2Bcontrol','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19900060623&hterms=feedforward+control&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dfeedforward%2Bcontrol"><span>Feedforward/feedback control synthesis for performance and <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wie, Bong; Liu, Qiang</p> <p>1990-01-01</p> <p>Both feedforward and feedback control approaches for uncertain dynamical systems are investigated. The control <span class="hlt">design</span> objective is to achieve a fast settling time (high performance) and <span class="hlt">robustness</span> (insensitivity) to plant modeling uncertainty. Preshapong of an ideal, time-optimal control input using a 'tapped-delay' filter is shown to provide a rapid maneuver with <span class="hlt">robust</span> performance. A <span class="hlt">robust</span>, non-minimum-phase feedback controller is synthesized with particular emphasis on its proper implementation for a non-zero set-point control problem. The proposed feedforward/feedback control approach is <span class="hlt">robust</span> for a certain class of uncertain dynamical systems, since the control input command computed for a given desired output does not depend on the plant parameters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/11764251','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/11764251"><span>Using open <span class="hlt">robust</span> <span class="hlt">design</span> models to estimate temporary emigration from capture-recapture data.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kendall, W L; Bjorkland, R</p> <p>2001-12-01</p> <p>Capture-recapture studies are crucial in many circumstances for estimating demographic parameters for wildlife and fish populations. Pollock's <span class="hlt">robust</span> <span class="hlt">design</span>, involving multiple sampling occasions per period of interest, provides several advantages over classical approaches. This includes the ability to estimate the probability of being present and available for detection, which in some situations is equivalent to breeding probability. We present a model for estimating availability for detection that relaxes two assumptions required in previous approaches. The first is that the sampled population is closed to additions and deletions across samples within a period of interest. The second is that each member of the population has the same probability of being available for detection in a given period. We apply our model to estimate survival and breeding probability in a study of hawksbill sea turtles (Eretmochelys imbricata), where previous approaches are not appropriate.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www3.interscience.wiley.com/journal/119016760/abstract+;+http://www3.interscience.wiley.com/cgi-bin/fulltext/119016760/PDFSTART','USGSPUBS'); return false;" href="http://www3.interscience.wiley.com/journal/119016760/abstract+;+http://www3.interscience.wiley.com/cgi-bin/fulltext/119016760/PDFSTART"><span>Using open <span class="hlt">robust</span> <span class="hlt">design</span> models to estimate temporary emigration from capture-recapture data</span></a></p> <p><a target="_blank" href="http://pubs.er.usgs.gov/pubs/index.jsp?view=adv">USGS Publications Warehouse</a></p> <p>Kendall, W.L.; Bjorkland, R.</p> <p>2001-01-01</p> <p>Capture-recapture studies are crucial in many circumstances for estimating demographic parameters for wildlife and fish populations. Pollock's <span class="hlt">robust</span> <span class="hlt">design</span>, involving multiple sampling occasions per period of interest, provides several advantages over classical approaches. This includes the ability to estimate the probability of being present and available for detection, which in some situations is equivalent to breeding probability. We present a model for estimating availability for detection that relaxes two assumptions required in previous approaches. The first is that the sampled population is closed to additions and deletions across samples within a period of interest. The second is that each member of the population has the same probability of being available for detection in a given period. We apply our model to estimate survival and breeding probability in a study of hawksbill sea turtles (Eretmochelys imbricata), where previous approaches are not appropriate.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19413756','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19413756"><span><span class="hlt">Robust</span> experimental <span class="hlt">design</span> for optimizing the microbial inhibitor test for penicillin detection in milk.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nagel, O G; Molina, M P; Basílico, J C; Zapata, M L; Althaus, R L</p> <p>2009-06-01</p> <p>To use experimental <span class="hlt">design</span> techniques and a multiple logistic regression model to optimize a microbiological inhibition test with dichotomous response for the detection of Penicillin G in milk. A 2(3) x 2(2) <span class="hlt">robust</span> experimental <span class="hlt">design</span> with two replications was used. The effects of three control factors (V: culture medium volume, S: spore concentration of Geobacillus stearothermophilus, I: indicator concentration), two noise factors (Dt: diffusion time, Ip: incubation period) and their interactions were studied. The V, S, Dt, Ip factors and V x S, V x Ip, S x Ip interactions showed significant effects. The use of 100 microl culture medium volume, 2 x 10(5) spores ml(-1), 60 min diffusion time and 3 h incubation period is recommended. In these elaboration conditions, the penicillin detection limit was of 3.9 microg l(-1), similar to the maximum residue limit (MRL). Of the two noise factors studied, the incubation period can be controlled by means of the culture medium volume and spore concentration. We were able to optimize bioassays of dichotomous response using an experimental <span class="hlt">design</span> and logistic regression model for the detection of residues at the level of MRL, aiding in the avoidance of health problems in the consumer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017SPIE10459E..0YK','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017SPIE10459E..0YK"><span><span class="hlt">Robust</span> <span class="hlt">design</span> study on the wide angle lens with free distortion for mobile lens</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Taeyoung; Yong, Liu; Xu, Qing</p> <p>2017-10-01</p> <p>Recently new trend applying wide angle in mobile imaging lens is attracting. Specially, customer requirements for capturing wider scene result that a field of view of lens be wider than 100deg. Introduction of retro-focus type lens in mobile imaging lens is required. However, imaging lens in mobile phone always face to many constraints such as lower total length, low F/# and higher performance. The sensitivity for fabrication may become more severe because of wide angle FOV. In this paper, we investigate an optical lens <span class="hlt">design</span> satisfy all requirements for mobile imaging lens. In order to accomplish Low cost and small depth of optical system, we used plastic materials for all element and the productivity is considered for realization. The lateral color is minimized less than 2 pixels and optical distortion is less than 5%. Also, we divided optical system into 2 part for <span class="hlt">robust</span> <span class="hlt">design</span>. The compensation between 2 groups can help us to increase yield in practice. The 2 group alignment for high yield may be a promising solution for wide angle lens.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21458628','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21458628"><span>Application of new methodologies based on <span class="hlt">design</span> of experiments, independent component analysis and <span class="hlt">design</span> space for <span class="hlt">robust</span> optimization in liquid chromatography.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Debrus, Benjamin; Lebrun, Pierre; Ceccato, Attilio; Caliaro, Gabriel; Rozet, Eric; Nistor, Iolanda; Oprean, Radu; Rupérez, Francisco J; Barbas, Coral; Boulanger, Bruno; Hubert, Philippe</p> <p>2011-04-08</p> <p>HPLC separations of an unknown sample mixture and a pharmaceutical formulation have been optimized using a recently developed chemometric methodology proposed by W. Dewé et al. in 2004 and improved by P. Lebrun et al. in 2008. This methodology is based on experimental <span class="hlt">designs</span> which are used to model retention times of compounds of interest. Then, the prediction accuracy and the optimal separation <span class="hlt">robustness</span>, including the uncertainty study, were evaluated. Finally, the <span class="hlt">design</span> space (ICH Q8(R1) guideline) was computed as the probability for a criterion to lie in a selected range of acceptance. Furthermore, the chromatograms were automatically read. Peak detection and peak matching were carried out with a previously developed methodology using independent component analysis published by B. Debrus et al. in 2009. The present successful applications strengthen the high potential of these methodologies for the automated development of chromatographic methods. Copyright © 2011 Elsevier B.V. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960034349','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960034349"><span>UNIX-based operating systems <span class="hlt">robustness</span> evaluation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chang, Yu-Ming</p> <p>1996-01-01</p> <p><span class="hlt">Robust</span> operating systems are required for reliable computing. Techniques for <span class="hlt">robustness</span> evaluation of operating systems not only enhance the understanding of the reliability of computer systems, but also provide valuable feed- back to system <span class="hlt">designers</span>. This thesis presents results from <span class="hlt">robustness</span> evaluation experiments on five UNIX-based operating systems, which include Digital Equipment's OSF/l, Hewlett Packard's HP-UX, Sun Microsystems' Solaris and SunOS, and Silicon Graphics' IRIX. Three sets of experiments were performed. The methodology for evaluation tested (1) the exception handling mechanism, (2) system resource management, and (3) system capacity under high workload stress. An exception generator was used to evaluate the exception handling mechanism of the operating systems. Results included exit status of the exception generator and the system state. Resource management techniques used by individual operating systems were tested using programs <span class="hlt">designed</span> to usurp system resources such as physical memory and process slots. Finally, the workload stress testing evaluated the effect of the workload on system performance by running a synthetic workload and recording the response time of local and remote user requests. Moderate to severe performance degradations were observed on the systems under stress.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20090002564','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20090002564"><span><span class="hlt">Robust</span>, optimal subsonic airfoil shapes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rai, Man Mohan (Inventor)</p> <p>2008-01-01</p> <p>Method system, and product from application of the method, for <span class="hlt">design</span> of a subsonic airfoil shape, beginning with an arbitrary initial airfoil shape and incorporating one or more constraints on the airfoil geometric parameters and flow characteristics. The resulting <span class="hlt">design</span> is <span class="hlt">robust</span> against variations in airfoil dimensions and local airfoil shape introduced in the airfoil manufacturing process. A perturbation procedure provides a class of airfoil shapes, beginning with an initial airfoil shape.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900013712','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900013712"><span>A methodology for formulating a minimal uncertainty model for <span class="hlt">robust</span> control system <span class="hlt">design</span> and analysis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Belcastro, Christine M.; Chang, B.-C.; Fischl, Robert</p> <p>1989-01-01</p> <p>In the <span class="hlt">design</span> and analysis of <span class="hlt">robust</span> control systems for uncertain plants, the technique of formulating what is termed an M-delta model has become widely accepted and applied in the <span class="hlt">robust</span> control literature. The M represents the transfer function matrix M(s) of the nominal system, and delta represents an uncertainty matrix acting on M(s). The uncertainty can arise from various sources, such as structured uncertainty from parameter variations or multiple unstructured uncertainties from unmodeled dynamics and other neglected phenomena. In general, delta is a block diagonal matrix, and for real parameter variations the diagonal elements are real. As stated in the literature, this structure can always be formed for any linear interconnection of inputs, outputs, transfer functions, parameter variations, and perturbations. However, very little of the literature addresses methods for obtaining this structure, and none of this literature addresses a general methodology for obtaining a minimal M-delta model for a wide class of uncertainty. Since have a delta matrix of minimum order would improve the efficiency of structured singular value (or multivariable stability margin) computations, a method of obtaining a minimal M-delta model would be useful. A generalized method of obtaining a minimal M-delta structure for systems with real parameter variations is given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012APS..DPPUP8053W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012APS..DPPUP8053W"><span>The conceptual <span class="hlt">design</span> of a <span class="hlt">robust</span>, compact, modular tokamak reactor based on high-field superconductors</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Whyte, D. G.; Bonoli, P.; Barnard, H.; Haakonsen, C.; Hartwig, Z.; Kasten, C.; Palmer, T.; Sung, C.; Sutherland, D.; Bromberg, L.; Mangiarotti, F.; Goh, J.; Sorbom, B.; Sierchio, J.; Ball, J.; Greenwald, M.; Olynyk, G.; Minervini, J.</p> <p>2012-10-01</p> <p>Two of the greatest challenges to tokamak reactors are 1) large single-unit cost of each reactor's construction and 2) their susceptibility to disruptions from operation at or above operational limits. We present an attractive tokamak reactor <span class="hlt">design</span> that substantially lessens these issues by exploiting recent advancements in superconductor (SC) tapes allowing peak field on SC coil > 20 Tesla. A R˜3.3 m, B˜9.2 T, ˜ 500 MW fusion power tokamak provides high fusion gain while avoiding all disruptive operating boundaries (no-wall beta, kink, and density limits). <span class="hlt">Robust</span> steady-state core scenarios are obtained by exploiting the synergy of high field, compact size and ideal efficiency current drive using high-field side launch of Lower Hybrid waves. The <span class="hlt">design</span> features a completely modular replacement of internal solid components enabled by the demountability of the coils/tapes and the use of an immersion liquid blanket. This modularity opens up the possibility of using the device as a nuclear component test facility.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.908a2009M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.908a2009M"><span>Evaluation on the feasibility of using bamboo fillers in plastic gear manufacturing via the <span class="hlt">Taguchi</span> optimization method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mehat, N. M.; Kamaruddin, S.</p> <p>2017-10-01</p> <p>An increase in demand for industrial gears has instigated the escalating uses of plastic-matrix composites, particularly carbon or glass fibre reinforced plastics as gear material to enhance the properties and limitation in plastic gears. However, the production of large quantity of these synthetic fibres reinforced composites has posed serious threat to ecosystem. Therefore, this work is conducted to study the applicability and practical ability of using bamboo fillers particularly in plastic gear manufacturing as opposed to synthetic fibres via the <span class="hlt">Taguchi</span> optimization method. The results showed that no failure mechanism such as gear tooth root cracking and severe tooth wear were observed in gear tested made of 5-30 wt% of bamboo fillers in comparing with the unfilled PP gear. These results indicated that bamboo can be practically and economically used as an alternative filler in plastic material reinforcement as well as in minimizing the cost of raw material in general.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1855b0015S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1855b0015S"><span>Application of <span class="hlt">Taguchi</span>-grey method to optimize drilling of EMS 45 steel using minimum quantity lubrication (MQL) with multiple performance characteristics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Soepangkat, Bobby O. P.; Suhardjono, Pramujati, Bambang</p> <p>2017-06-01</p> <p>Machining under minimum quantity lubrication (MQL) has drawn the attention of researchers as an alternative to the traditionally used wet and dry machining conditions with the purpose to minimize the cooling and lubricating cost, as well as to reduce cutting zone temperature, tool wear, and hole surface roughness. Drilling is one of the important operations to assemble machine components. The objective of this study was to optimize drilling parameters such as cutting feed and cutting speed, drill type and drill point angle on the thrust force, torque, hole surface roughness and tool flank wear in drilling EMS 45 tool steel using MQL. In this study, experiments were carried out as per <span class="hlt">Taguchi</span> <span class="hlt">design</span> of experiments while an L18 orthogonal array was used to study the influence of various combinations of drilling parameters and tool geometries on the thrust force, torque, hole surface roughness and tool flank wear. The optimum drilling parameters was determined by using grey relational grade obtained from grey relational analysis for multiple-performance characteristics. The drilling experiments were carried out by using twist drill and CNC machining center. This work is useful for optimum values selection of various drilling parameters and tool geometries that would not only minimize the thrust force and torque, but also reduce hole surface roughness and tool flank wear.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4032542','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4032542"><span>Topological properties of <span class="hlt">robust</span> biological and computational networks</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Navlakha, Saket; He, Xin; Faloutsos, Christos; Bar-Joseph, Ziv</p> <p>2014-01-01</p> <p>Network <span class="hlt">robustness</span> is an important principle in biology and engineering. Previous studies of global networks have identified both redundancy and sparseness as topological properties used by <span class="hlt">robust</span> networks. By focusing on molecular subnetworks, or modules, we show that module topology is tightly linked to the level of environmental variability (noise) the module expects to encounter. Modules internal to the cell that are less exposed to environmental noise are more connected and less <span class="hlt">robust</span> than external modules. A similar <span class="hlt">design</span> principle is used by several other biological networks. We propose a simple change to the evolutionary gene duplication model which gives rise to the rich range of module topologies observed within real networks. We apply these observations to evaluate and <span class="hlt">design</span> communication networks that are specifically optimized for noisy or malicious environments. Combined, joint analysis of biological and computational networks leads to novel algorithms and insights benefiting both fields. PMID:24789562</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013IJC....86.1620M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013IJC....86.1620M"><span>Integrated direct/indirect adaptive <span class="hlt">robust</span> motion trajectory tracking control of pneumatic cylinders</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Meng, Deyuan; Tao, Guoliang; Zhu, Xiaocong</p> <p>2013-09-01</p> <p>This paper studies the precision motion trajectory tracking control of a pneumatic cylinder driven by a proportional-directional control valve. An integrated direct/indirect adaptive <span class="hlt">robust</span> controller is proposed. The controller employs a physical model based indirect-type parameter estimation to obtain reliable estimates of unknown model parameters, and utilises a <span class="hlt">robust</span> control method with dynamic compensation type fast adaptation to attenuate the effects of parameter estimation errors, unmodelled dynamics and disturbances. Due to the use of projection mapping, the <span class="hlt">robust</span> control law and the parameter adaption algorithm can be <span class="hlt">designed</span> separately. Since the system model uncertainties are unmatched, the recursive backstepping technology is adopted to <span class="hlt">design</span> the <span class="hlt">robust</span> control law. Extensive comparative experimental results are presented to illustrate the effectiveness of the proposed controller and its performance <span class="hlt">robustness</span> to parameter variations and sudden disturbances.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_22 --> <div id="page_23" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="441"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA612737','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA612737"><span><span class="hlt">Robust</span> Network <span class="hlt">Design</span> - Connectivity and Beyond</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2015-01-15</p> <p>utilize a heterogeneous set of physical links (RF, Optical/Laser and SATCOM), for interconnecting a set of terrestrial, space and highly mobile airborne...<span class="hlt">design</span> of mobility patterns of airborne platforms to provide stable operating conditions,  the <span class="hlt">design</span> of networks that enable graceful performance...research effort, Airborne Network research was primarily directed towards Mobile Ad-hoc Networks (MANET). From our experience in <span class="hlt">design</span> and</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930012455','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930012455"><span><span class="hlt">Robust</span> on-off pulse control of flexible space vehicles</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Wie, Bong; Sinha, Ravi</p> <p>1993-01-01</p> <p>The on-off reaction jet control system is often used for attitude and orbital maneuvering of various spacecraft. Future space vehicles such as the orbital transfer vehicles, orbital maneuvering vehicles, and space station will extensively use reaction jets for orbital maneuvering and attitude stabilization. The proposed <span class="hlt">robust</span> fuel- and time-optimal control algorithm is used for a three-mass spacing model of flexible spacecraft. A fuel-efficient on-off control logic is developed for <span class="hlt">robust</span> rest-to-rest maneuver of a flexible vehicle with minimum excitation of structural modes. The first part of this report is concerned with the problem of selecting a proper pair of jets for practical trade-offs among the maneuvering time, fuel consumption, structural mode excitation, and performance <span class="hlt">robustness</span>. A time-optimal control problem subject to parameter <span class="hlt">robustness</span> constraints is formulated and solved. The second part of this report deals with obtaining parameter insensitive fuel- and time- optimal control inputs by solving a constrained optimization problem subject to <span class="hlt">robustness</span> constraints. It is shown that sensitivity to modeling errors can be significantly reduced by the proposed, robustified open-loop control approach. The final part of this report deals with sliding mode control <span class="hlt">design</span> for uncertain flexible structures. The benchmark problem of a flexible structure is used as an example for the feedback sliding mode controller <span class="hlt">design</span> with bounded control inputs and <span class="hlt">robustness</span> to parameter variations is investigated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ChJME..29..739W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ChJME..29..739W"><span>Vehicle active steering control research based on two-DOF <span class="hlt">robust</span> internal model control</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wu, Jian; Liu, Yahui; Wang, Fengbo; Bao, Chunjiang; Sun, Qun; Zhao, Youqun</p> <p>2016-07-01</p> <p>Because of vehicle's external disturbances and model uncertainties, <span class="hlt">robust</span> control algorithms have obtained popularity in vehicle stability control. The <span class="hlt">robust</span> control usually gives up performance in order to guarantee the <span class="hlt">robustness</span> of the control algorithm, therefore an improved <span class="hlt">robust</span> internal model control(IMC) algorithm blending model tracking and internal model control is put forward for active steering system in order to reach high performance of yaw rate tracking with certain <span class="hlt">robustness</span>. The proposed algorithm inherits the good model tracking ability of the IMC control and guarantees <span class="hlt">robustness</span> to model uncertainties. In order to separate the <span class="hlt">design</span> process of model tracking from the <span class="hlt">robustness</span> <span class="hlt">design</span> process, the improved 2 degree of freedom(DOF) <span class="hlt">robust</span> internal model controller structure is given from the standard Youla parameterization. Simulations of double lane change maneuver and those of crosswind disturbances are conducted for evaluating the <span class="hlt">robust</span> control algorithm, on the basis of a nonlinear vehicle simulation model with a magic tyre model. Results show that the established 2-DOF <span class="hlt">robust</span> IMC method has better model tracking ability and a guaranteed level of <span class="hlt">robustness</span> and <span class="hlt">robust</span> performance, which can enhance the vehicle stability and handling, regardless of variations of the vehicle model parameters and the external crosswind interferences. Contradiction between performance and <span class="hlt">robustness</span> of active steering control algorithm is solved and higher control performance with certain <span class="hlt">robustness</span> to model uncertainties is obtained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17544426','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17544426"><span>A novel <span class="hlt">robust</span> speed controller scheme for PMBLDC motor.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Thirusakthimurugan, P; Dananjayan, P</p> <p>2007-10-01</p> <p>The <span class="hlt">design</span> of speed and position controllers for permanent magnet brushless DC motor (PMBLDC) drive remains as an open problem in the field of motor drives. A precise speed control of PMBLDC motor is complex due to nonlinear coupling between winding currents and rotor speed. In addition, the nonlinearity present in the developed torque due to magnetic saturation of the rotor further complicates this issue. This paper presents a novel control scheme to the conventional PMBLDC motor drive, which aims at improving the <span class="hlt">robustness</span> by complete decoupling of the <span class="hlt">design</span> besides minimizing the mutual influence among the speed and current control loops. The interesting feature of this <span class="hlt">robust</span> control scheme is its suitability for both static and dynamic aspects. The effectiveness of the proposed <span class="hlt">robust</span> speed control scheme is verified through simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19386410','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19386410"><span>Info-gap theory and <span class="hlt">robust</span> <span class="hlt">design</span> of surveillance for invasive species: the case study of Barrow Island.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Davidovitch, Lior; Stoklosa, Richard; Majer, Jonathan; Nietrzeba, Alex; Whittle, Peter; Mengersen, Kerrie; Ben-Haim, Yakov</p> <p>2009-06-01</p> <p>Surveillance for invasive non-indigenous species (NIS) is an integral part of a quarantine system. Estimating the efficiency of a surveillance strategy relies on many uncertain parameters estimated by experts, such as the efficiency of its components in face of the specific NIS, the ability of the NIS to inhabit different environments, and so on. Due to the importance of detecting an invasive NIS within a critical period of time, it is crucial that these uncertainties be accounted for in the <span class="hlt">design</span> of the surveillance system. We formulate a detection model that takes into account, in addition to structured sampling for incursive NIS, incidental detection by untrained workers. We use info-gap theory for satisficing (not minimizing) the probability of detection, while at the same time maximizing the <span class="hlt">robustness</span> to uncertainty. We demonstrate the trade-off between <span class="hlt">robustness</span> to uncertainty, and an increase in the required probability of detection. An empirical example based on the detection of Pheidole megacephala on Barrow Island demonstrates the use of info-gap analysis to select a surveillance strategy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=definition+AND+Science&pg=7&id=EJ1005963','ERIC'); return false;" href="https://eric.ed.gov/?q=definition+AND+Science&pg=7&id=EJ1005963"><span>Mental Models: A <span class="hlt">Robust</span> Definition</span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Rook, Laura</p> <p>2013-01-01</p> <p>Purpose: The concept of a mental model has been described by theorists from diverse disciplines. The purpose of this paper is to offer a <span class="hlt">robust</span> definition of an individual mental model for use in organisational management. <span class="hlt">Design</span>/methodology/approach: The approach adopted involves an interdisciplinary literature review of disciplines, including…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19860021260','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19860021260"><span><span class="hlt">Robust</span> detection, isolation and accommodation for sensor failures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Emami-Naeini, A.; Akhter, M. M.; Rock, S. M.</p> <p>1986-01-01</p> <p>The objective is to extend the recent advances in <span class="hlt">robust</span> control system <span class="hlt">design</span> of multivariable systems to sensor failure detection, isolation, and accommodation (DIA), and estimator <span class="hlt">design</span>. This effort provides analysis tools to quantify the trade-off between performance <span class="hlt">robustness</span> and DIA sensitivity, which are to be used to achieve higher levels of performance <span class="hlt">robustness</span> for given levels of DIA sensitivity. An innovations-based DIA scheme is used. Estimators, which depend upon a model of the process and process inputs and outputs, are used to generate these innovations. Thresholds used to determine failure detection are computed based on bounds on modeling errors, noise properties, and the class of failures. The applicability of the newly developed tools are demonstrated on a multivariable aircraft turbojet engine example. A new concept call the threshold selector was developed. It represents a significant and innovative tool for the analysis and synthesis of DiA algorithms. The estimators were made <span class="hlt">robust</span> by introduction of an internal model and by frequency shaping. The internal mode provides asymptotically unbiased filter estimates.The incorporation of frequency shaping of the Linear Quadratic Gaussian cost functional modifies the estimator <span class="hlt">design</span> to make it suitable for sensor failure DIA. The results are compared with previous studies which used thresholds that were selcted empirically. Comparison of these two techniques on a nonlinear dynamic engine simulation shows improved performance of the new method compared to previous techniques</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930019435','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930019435"><span>Soft computing in <span class="hlt">design</span> and manufacturing of advanced materials</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cios, Krzysztof J.; Baaklini, George Y; Vary, Alex</p> <p>1993-01-01</p> <p>The potential of fuzzy sets and neural networks, often referred to as soft computing, for aiding in all aspects of manufacturing of advanced materials like ceramics is addressed. In <span class="hlt">design</span> and manufacturing of advanced materials, it is desirable to find which of the many processing variables contribute most to the desired properties of the material. There is also interest in real time quality control of parameters that govern material properties during processing stages. The concepts of fuzzy sets and neural networks are briefly introduced and it is shown how they can be used in the <span class="hlt">design</span> and manufacturing processes. These two computational methods are alternatives to other methods such as the <span class="hlt">Taguchi</span> method. The two methods are demonstrated by using data collected at NASA Lewis Research Center. Future research directions are also discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27227724','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27227724"><span>Data-Adaptive Bias-Reduced Doubly <span class="hlt">Robust</span> Estimation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Vermeulen, Karel; Vansteelandt, Stijn</p> <p>2016-05-01</p> <p>Doubly <span class="hlt">robust</span> estimators have now been proposed for a variety of target parameters in the causal inference and missing data literature. These consistently estimate the parameter of interest under a semiparametric model when one of two nuisance working models is correctly specified, regardless of which. The recently proposed bias-reduced doubly <span class="hlt">robust</span> estimation procedure aims to partially retain this <span class="hlt">robustness</span> in more realistic settings where both working models are misspecified. These so-called bias-reduced doubly <span class="hlt">robust</span> estimators make use of special (finite-dimensional) nuisance parameter estimators that are <span class="hlt">designed</span> to locally minimize the squared asymptotic bias of the doubly <span class="hlt">robust</span> estimator in certain directions of these finite-dimensional nuisance parameters under misspecification of both parametric working models. In this article, we extend this idea to incorporate the use of data-adaptive estimators (infinite-dimensional nuisance parameters), by exploiting the bias reduction estimation principle in the direction of only one nuisance parameter. We additionally provide an asymptotic linearity theorem which gives the influence function of the proposed doubly <span class="hlt">robust</span> estimator under correct specification of a parametric nuisance working model for the missingness mechanism/propensity score but a possibly misspecified (finite- or infinite-dimensional) outcome working model. Simulation studies confirm the desirable finite-sample performance of the proposed estimators relative to a variety of other doubly <span class="hlt">robust</span> estimators.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..342a2005A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..342a2005A"><span>Integration of Mahalanobis-<span class="hlt">Taguchi</span> system and traditional cost accounting for remanufacturing crankshaft</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Abu, M. Y.; Norizan, N. S.; Rahman, M. S. Abd</p> <p>2018-04-01</p> <p>Remanufacturing is a sustainability strategic planning which transforming the end of life product to as new performance with their warranty is same or better than the original product. In order to quantify the advantages of this strategy, all the processes must implement the optimization to reach the ultimate goal and reduce the waste generated. The aim of this work is to evaluate the criticality of parameters on the end of life crankshaft based on Taguchi’s orthogonal array. Then, estimate the cost using traditional cost accounting by considering the critical parameters. By implementing the optimization, the remanufacturer obviously produced lower cost and waste during production with higher potential to gain the profit. Mahalanobis-<span class="hlt">Taguchi</span> System was proven as a powerful method of optimization that revealed the criticality of parameters. When subjected the method to the MAN engine model, there was 5 out of 6 crankpins were critical which need for grinding process while no changes happened to the Caterpillar engine model. Meanwhile, the cost per unit for MAN engine model was changed from MYR1401.29 to RM1251.29 while for Caterpillar engine model have no changes due to the no changes on criticality of parameters consideration. Therefore, by integrating the optimization and costing through remanufacturing process, a better decision can be achieved after observing the potential profit will be gained. The significant of output demonstrated through promoting sustainability by reducing re-melting process of damaged parts to ensure consistent benefit of return cores.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..374a2054T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..374a2054T"><span>The <span class="hlt">Taguchi</span> Method Application to Improve the Quality of a Sustainable Process</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Titu, A. M.; Sandu, A. V.; Pop, A. B.; Titu, S.; Ciungu, T. C.</p> <p>2018-06-01</p> <p>Taguchi’s method has always been a method used to improve the quality of the analyzed processes and products. This research shows an unusual situation, namely the modeling of some parameters, considered technical parameters, in a process that is wanted to be durable by improving the quality process and by ensuring quality using an experimental research method. Modern experimental techniques can be applied in any field and this study reflects the benefits of interacting between the agriculture sustainability principles and the Taguchi’s Method application. The experimental method used in this practical study consists of combining engineering techniques with experimental statistical modeling to achieve rapid improvement of quality costs, in fact seeking optimization at the level of existing processes and the main technical parameters. The paper is actually a purely technical research that promotes a technical experiment using the <span class="hlt">Taguchi</span> method, considered to be an effective method since it allows for rapid achievement of 70 to 90% of the desired optimization of the technical parameters. The missing 10 to 30 percent can be obtained with one or two complementary experiments, limited to 2 to 4 technical parameters that are considered to be the most influential. Applying the Taguchi’s Method in the technique and not only, allowed the simultaneous study in the same experiment of the influence factors considered to be the most important in different combinations and, at the same time, determining each factor contribution.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhyA..490..601Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhyA..490..601Z"><span>Dynamic <span class="hlt">robustness</span> of knowledge collaboration network of open source product development community</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhou, Hong-Li; Zhang, Xiao-Dong</p> <p>2018-01-01</p> <p>As an emergent innovative <span class="hlt">design</span> style, open source product development communities are characterized by a self-organizing, mass collaborative, networked structure. The <span class="hlt">robustness</span> of the community is critical to its performance. Using the complex network modeling method, the knowledge collaboration network of the community is formulated, and the <span class="hlt">robustness</span> of the network is systematically and dynamically studied. The characteristics of the network along the development period determine that its <span class="hlt">robustness</span> should be studied from three time stages: the start-up, development and mature stages of the network. Five kinds of user-loss pattern are <span class="hlt">designed</span>, to assess the network's <span class="hlt">robustness</span> under different situations in each of these three time stages. Two indexes - the largest connected component and the network efficiency - are used to evaluate the <span class="hlt">robustness</span> of the community. The proposed approach is applied in an existing open source car <span class="hlt">design</span> community. The results indicate that the knowledge collaboration networks show different levels of <span class="hlt">robustness</span> in different stages and different user loss patterns. Such analysis can be applied to provide protection strategies for the key users involved in knowledge dissemination and knowledge contribution at different stages of the network, thereby promoting the sustainable and stable development of the open source community.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014IJSyS..45.1869J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014IJSyS..45.1869J"><span><span class="hlt">Robust</span> consensus algorithm for multi-agent systems with exogenous disturbances under convergence conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jiang, Yulian; Liu, Jianchang; Tan, Shubin; Ming, Pingsong</p> <p>2014-09-01</p> <p>In this paper, a <span class="hlt">robust</span> consensus algorithm is developed and sufficient conditions for convergence to consensus are proposed for a multi-agent system (MAS) with exogenous disturbances subject to partial information. By utilizing H∞ <span class="hlt">robust</span> control, differential game theory and a <span class="hlt">design</span>-based approach, the consensus problem of the MAS with exogenous bounded interference is resolved and the disturbances are restrained, simultaneously. Attention is focused on <span class="hlt">designing</span> an H∞ <span class="hlt">robust</span> controller (the <span class="hlt">robust</span> consensus algorithm) based on minimisation of our proposed rational and individual cost functions according to goals of the MAS. Furthermore, sufficient conditions for convergence of the <span class="hlt">robust</span> consensus algorithm are given. An example is employed to demonstrate that our results are effective and more capable to restrain exogenous disturbances than the existing literature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JQSRT.209..129C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JQSRT.209..129C"><span><span class="hlt">Robust</span> optimization of a tandem grating solar thermal absorber</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Choi, Jongin; Kim, Mingeon; Kang, Kyeonghwan; Lee, Ikjin; Lee, Bong Jae</p> <p>2018-04-01</p> <p>Ideal solar thermal absorbers need to have a high value of the spectral absorptance in the broad solar spectrum to utilize the solar radiation effectively. Majority of recent studies about solar thermal absorbers focus on achieving nearly perfect absorption using nanostructures, whose characteristic dimension is smaller than the wavelength of sunlight. However, precise fabrication of such nanostructures is not easy in reality; that is, unavoidable errors always occur to some extent in the dimension of fabricated nanostructures, causing an undesirable deviation of the absorption performance between the <span class="hlt">designed</span> structure and the actually fabricated one. In order to minimize the variation in the solar absorptance due to the fabrication error, the <span class="hlt">robust</span> optimization can be performed during the <span class="hlt">design</span> process. However, the optimization of solar thermal absorber considering all <span class="hlt">design</span> variables often requires tremendous computational costs to find an optimum combination of <span class="hlt">design</span> variables with the <span class="hlt">robustness</span> as well as the high performance. To achieve this goal, we apply the <span class="hlt">robust</span> optimization using the Kriging method and the genetic algorithm for <span class="hlt">designing</span> a tandem grating solar absorber. By constructing a surrogate model through the Kriging method, computational cost can be substantially reduced because exact calculation of the performance for every combination of variables is not necessary. Using the surrogate model and the genetic algorithm, we successfully <span class="hlt">design</span> an effective solar thermal absorber exhibiting a low-level of performance degradation due to the fabrication uncertainty of <span class="hlt">design</span> variables.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4845795','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4845795"><span>The developmental genetics of biological <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Mestek Boukhibar, Lamia; Barkoulas, Michalis</p> <p>2016-01-01</p> <p>Background Living organisms are continuously confronted with perturbations, such as environmental changes that include fluctuations in temperature and nutrient availability, or genetic changes such as mutations. While some developmental systems are affected by such challenges and display variation in phenotypic traits, others continue consistently to produce invariable phenotypes despite perturbation. This ability of a living system to maintain an invariable phenotype in the face of perturbations is termed developmental <span class="hlt">robustness</span>. Biological <span class="hlt">robustness</span> is a phenomenon observed across phyla, and studying its mechanisms is central to deciphering the genotype–phenotype relationship. Recent work in yeast, animals and plants has shown that <span class="hlt">robustness</span> is genetically controlled and has started to reveal the underlying mechinisms behind it. Scope and Conclusions Studying biological <span class="hlt">robustness</span> involves focusing on an important property of developmental traits, which is the phenotypic distribution within a population. This is often neglected because the vast majority of developmental biology studies instead focus on population aggregates, such as trait averages. By drawing on findings in animals and yeast, this Viewpoint considers how studies on plant developmental <span class="hlt">robustness</span> may benefit from strict definitions of what is the developmental system of choice and what is the relevant perturbation, and also from clear distinctions between gene effects on the trait mean and the trait variance. Recent advances in quantitative developmental biology and high-throughput phenotyping now allow the <span class="hlt">design</span> of targeted genetic screens to identify genes that amplify or restrict developmental trait variance and to study how variation propagates across different phenotypic levels in biological systems. The molecular characterization of more quantitative trait loci affecting trait variance will provide further insights into the evolution of genes modulating developmental <span class="hlt">robustness</span>. The</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.885a2010T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.885a2010T"><span>Multi objective <span class="hlt">Taguchi</span> optimization approach for resistance spot welding of cold rolled TWIP steel sheets</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tutar, Mumin; Aydin, Hakan; Bayram, Ali</p> <p>2017-08-01</p> <p>Formability and energy absorption capability of a steel sheet are highly desirable properties in manufacturing components for automotive applications. TWinning Induced Plastisity (TWIP) steels are, new generation high Mn alloyed steels, attractive for the automotive industry due to its outstanding elongation (%40-45) and tensile strength (~1000MPa). So, TWIP steels provide excellent formability and energy absorption capability. Another required property from the steel sheets is suitability for manufacturing methods such as welding. The use of the steel sheets in the automotive applications inevitably involves welding. Considering that there are 3000-5000 welded spots on a vehicle, it can be interpreted that one of the most important manufacturing method is Resistance Spot Welding (RSW) for the automotive industry. In this study; firstly, TWIP steel sheet were cold rolled to 15% reduction in thickness. Then, the cold rolled TWIP steel sheets were welded with RSW method. The welding parameters (welding current, welding time and electrode force) were optimized for maximizing the peak tensile shear load and minimizing the indentation of the joints using a <span class="hlt">Taguchi</span> L9 orthogonal array. The effect of welding parameters was also evaluated by examining the signal-to-noise ratio and analysis of variance (ANOVA) results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3541983','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3541983"><span>On the contributions of topological features to transcriptional regulatory network <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2012-01-01</p> <p>Background Because biological networks exhibit a high-degree of <span class="hlt">robustness</span>, a systemic understanding of their architecture and function requires an appraisal of the network <span class="hlt">design</span> principles that confer <span class="hlt">robustness</span>. In this project, we conduct a computational study of the contribution of three degree-based topological properties (transcription factor-target ratio, degree distribution, cross-talk suppression) and their combinations on the <span class="hlt">robustness</span> of transcriptional regulatory networks. We seek to quantify the relative degree of <span class="hlt">robustness</span> conferred by each property (and combination) and also to determine the extent to which these properties alone can explain the <span class="hlt">robustness</span> observed in transcriptional networks. Results To study individual properties and their combinations, we generated synthetic, random networks that retained one or more of the three properties with values derived from either the yeast or E. coli gene regulatory networks. <span class="hlt">Robustness</span> of these networks were estimated through simulation. Our results indicate that the combination of the three properties we considered explains the majority of the structural <span class="hlt">robustness</span> observed in the real transcriptional networks. Surprisingly, scale-free degree distribution is, overall, a minor contributor to <span class="hlt">robustness</span>. Instead, most <span class="hlt">robustness</span> is gained through topological features that limit the complexity of the overall network and increase the transcription factor subnetwork sparsity. Conclusions Our work demonstrates that (i) different types of <span class="hlt">robustness</span> are implemented by different topological aspects of the network and (ii) size and sparsity of the transcription factor subnetwork play an important role for <span class="hlt">robustness</span> induction. Our results are conserved across yeast and E Coli, which suggests that the <span class="hlt">design</span> principles examined are present within an array of living systems. PMID:23194062</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3995665','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3995665"><span>Biosorption of malachite green from aqueous solutions by Pleurotus ostreatus using <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p></p> <p>2014-01-01</p> <p>Dyes released into the environment have been posing a serious threat to natural ecosystems and aquatic life due to presence of heat, light, chemical and other exposures stable. In this study, the Pleurotus ostreatus (a macro-fungus) was used as a new biosorbent to study the biosorption of hazardous malachite green (MG) from aqueous solutions. The effective disposal of P. ostreatus is a meaningful work for environmental protection and maximum utilization of agricultural residues. The operational parameters such as biosorbent dose, pH, and ionic strength were investigated in a series of batch studies at 25°C. Freundlich isotherm model was described well for the biosorption equilibrium data. The biosorption process followed the pseudo-second-order kinetic model. <span class="hlt">Taguchi</span> method was used to simplify the experimental number for determining the significance of factors and the optimum levels of experimental factors for MG biosorption. Biosorbent dose and initial MG concentration had significant influences on the percent removal and biosorption capacity. The highest percent removal reached 89.58% and the largest biosorption capacity reached 32.33 mg/g. The Fourier transform infrared spectroscopy (FTIR) showed that the functional groups such as, carboxyl, hydroxyl, amino and phosphonate groups on the biosorbent surface could be the potential adsorption sites for MG biosorption. P. ostreatus can be considered as an alternative biosorbent for the removal of dyes from aqueous solutions. PMID:24620852</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24620852','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24620852"><span>Biosorption of malachite green from aqueous solutions by Pleurotus ostreatus using <span class="hlt">Taguchi</span> method.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Zhengsuo; Deng, Hongbo; Chen, Can; Yang, Ying; Xu, Heng</p> <p>2014-03-12</p> <p>Dyes released into the environment have been posing a serious threat to natural ecosystems and aquatic life due to presence of heat, light, chemical and other exposures stable. In this study, the Pleurotus ostreatus (a macro-fungus) was used as a new biosorbent to study the biosorption of hazardous malachite green (MG) from aqueous solutions. The effective disposal of P. ostreatus is a meaningful work for environmental protection and maximum utilization of agricultural residues.The operational parameters such as biosorbent dose, pH, and ionic strength were investigated in a series of batch studies at 25°C. Freundlich isotherm model was described well for the biosorption equilibrium data. The biosorption process followed the pseudo-second-order kinetic model. <span class="hlt">Taguchi</span> method was used to simplify the experimental number for determining the significance of factors and the optimum levels of experimental factors for MG biosorption. Biosorbent dose and initial MG concentration had significant influences on the percent removal and biosorption capacity. The highest percent removal reached 89.58% and the largest biosorption capacity reached 32.33 mg/g. The Fourier transform infrared spectroscopy (FTIR) showed that the functional groups such as, carboxyl, hydroxyl, amino and phosphonate groups on the biosorbent surface could be the potential adsorption sites for MG biosorption. P. ostreatus can be considered as an alternative biosorbent for the removal of dyes from aqueous solutions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29524765','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29524765"><span>Neural <span class="hlt">robust</span> stabilization via event-triggering mechanism and adaptive learning technique.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Wang, Ding; Liu, Derong</p> <p>2018-06-01</p> <p>The <span class="hlt">robust</span> control synthesis of continuous-time nonlinear systems with uncertain term is investigated via event-triggering mechanism and adaptive critic learning technique. We mainly focus on combining the event-triggering mechanism with adaptive critic <span class="hlt">designs</span>, so as to solve the nonlinear <span class="hlt">robust</span> control problem. This can not only make better use of computation and communication resources, but also conduct controller <span class="hlt">design</span> from the view of intelligent optimization. Through theoretical analysis, the nonlinear <span class="hlt">robust</span> stabilization can be achieved by obtaining an event-triggered optimal control law of the nominal system with a newly defined cost function and a certain triggering condition. The adaptive critic technique is employed to facilitate the event-triggered control <span class="hlt">design</span>, where a neural network is introduced as an approximator of the learning phase. The performance of the event-triggered <span class="hlt">robust</span> control scheme is validated via simulation studies and comparisons. The present method extends the application domain of both event-triggered control and adaptive critic control to nonlinear systems possessing dynamical uncertainties. Copyright © 2018 Elsevier Ltd. All rights reserved.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_23 --> <div id="page_24" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="461"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26713357','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26713357"><span><span class="hlt">Robust</span> <span class="hlt">Design</span> of a Particle-Free Silver-Organo-Complex Ink with High Conductivity and Inkjet Stability for Flexible Electronics.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Vaseem, Mohammad; McKerricher, Garret; Shamim, Atif</p> <p>2016-01-13</p> <p>Currently, silver-nanoparticle-based inkjet ink is commercially available. This type of ink has several serious problems such as a complex synthesis protocol, high cost, high sintering temperatures (∼200 °C), particle aggregation, nozzle clogging, poor shelf life, and jetting instability. For the emerging field of printed electronics, these shortcomings in conductive inks are barriers for their widespread use in practical applications. Formulating particle-free silver inks has potential to solve these issues and requires careful <span class="hlt">design</span> of the silver complexation. The ink complex must meet various requirements, such as in situ reduction, optimum viscosity, storage and jetting stability, smooth uniform sintered films, excellent adhesion, and high conductivity. This study presents a <span class="hlt">robust</span> formulation of silver-organo-complex (SOC) ink, where complexing molecules act as reducing agents. The 17 wt % silver loaded ink was printed and sintered on a wide range of substrates with uniform surface morphology and excellent adhesion. The jetting stability was monitored for 5 months to confirm that the ink was <span class="hlt">robust</span> and highly stable with consistent jetting performance. Radio frequency inductors, which are highly sensitive to metal quality, were demonstrated as a proof of concept on flexible PEN substrate. This is a major step toward producing high-quality electronic components with a <span class="hlt">robust</span> inkjet printing process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007EJASP2008..211C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007EJASP2008..211C"><span>A <span class="hlt">Robust</span> Zero-Watermarking Algorithm for Audio</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chen, Ning; Zhu, Jie</p> <p>2007-12-01</p> <p>In traditional watermarking algorithms, the insertion of watermark into the host signal inevitably introduces some perceptible quality degradation. Another problem is the inherent conflict between imperceptibility and <span class="hlt">robustness</span>. Zero-watermarking technique can solve these problems successfully. Instead of embedding watermark, the zero-watermarking technique extracts some essential characteristics from the host signal and uses them for watermark detection. However, most of the available zero-watermarking schemes are <span class="hlt">designed</span> for still image and their <span class="hlt">robustness</span> is not satisfactory. In this paper, an efficient and <span class="hlt">robust</span> zero-watermarking technique for audio signal is presented. The multiresolution characteristic of discrete wavelet transform (DWT), the energy compression characteristic of discrete cosine transform (DCT), and the Gaussian noise suppression property of higher-order cumulant are combined to extract essential features from the host audio signal and they are then used for watermark recovery. Simulation results demonstrate the effectiveness of our scheme in terms of inaudibility, detection reliability, and <span class="hlt">robustness</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MS%26E..352a2002Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MS%26E..352a2002Y"><span>Application of <span class="hlt">taguchi</span> method for selection parameter bleaching treatments against mechanical and physical properties of agave cantala fiber</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yudhanto, F.; Jamasri; Rochardjo, Heru S. B.</p> <p>2018-05-01</p> <p>The characterized agave cantala fiber in this research came from Sumenep, Madura, Indonesia was chemically processed using sodium hydroxide (NaOH) and hydrogen peroxide (H2O2) solution. The treatment with both solutions is called bleaching process. Tensile strength test of single fiber was used to get mechanical properties from selecting process of the various parameter are temperature, PH and concentration of H2O2 with an L9 orthogonal array by <span class="hlt">Taguchi</span> method. The results indicate that PH is most significant parameter influencing the tensile strength followed by temperature and concentration H2O2. The influence of bleaching treatment on tensile strength showed increasing of crystallinity index of fiber by 21%. It showed by lost of hemicellulose and lignin layers of fiber can be seen from waveforms changes of 1735 (C=O), 1627 (OH), 1319 (CH2), 1250 (C-O) by FTIR graph. The photo SEM showed that the bleaching of fibers causes the fibers more roughly and clearly than untreated fibers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://arc.engin.umich.edu/research/thrust-area-5.html','SCIGOVWS'); return false;" href="http://arc.engin.umich.edu/research/thrust-area-5.html"><span>Vehicle System Integration, Optimization, and <span class="hlt">Robustness</span></span></a></p> <p><a target="_blank" href="http://www.science.gov/aboutsearch.html">Science.gov Websites</a></p> <p></p> <p></p> <p><em>Operations</em> Technology Exchange Initiating Partnerships University Partners Government Partners Industry Contacts Researchers Thrust Area 5: Vehicle System Integration, <em>Optimization</em>, and <span class="hlt">Robustness</span> Thrust Area only optimal <span class="hlt">design</span> of the vehicle components, but also an <em>optimization</em> of the interactions between</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19920007094','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19920007094"><span><span class="hlt">Robust</span> control of systems with real parameter uncertainty and unmodelled dynamics</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chang, Bor-Chin; Fischl, Robert</p> <p>1991-01-01</p> <p>During this research period we have made significant progress in the four proposed areas: (1) <span class="hlt">design</span> of <span class="hlt">robust</span> controllers via H infinity optimization; (2) <span class="hlt">design</span> of <span class="hlt">robust</span> controllers via mixed H2/H infinity optimization; (3) M-delta structure and <span class="hlt">robust</span> stability analysis for structured uncertainties; and (4) a study on controllability and observability of perturbed plant. It is well known now that the two-Riccati-equation solution to the H infinity control problem can be used to characterize all possible stabilizing optimal or suboptimal H infinity controllers if the optimal H infinity norm or gamma, an upper bound of a suboptimal H infinity norm, is given. In this research, we discovered some useful properties of these H infinity Riccati solutions. Among them, the most prominent one is that the spectral radius of the product of these two Riccati solutions is a continuous, nonincreasing, convex function of gamma in the domain of interest. Based on these properties, quadratically convergent algorithms are developed to compute the optimal H infinity norm. We also set up a detailed procedure for applying the H infinity theory to <span class="hlt">robust</span> control systems <span class="hlt">design</span>. The desire to <span class="hlt">design</span> controllers with H infinity <span class="hlt">robustness</span> but H(exp 2) performance has recently resulted in mixed H(exp 2) and H infinity control problem formulation. The mixed H(exp 2)/H infinity problem have drawn the attention of many investigators. However, solution is only available for special cases of this problem. We formulated a relatively realistic control problem with H(exp 2) performance index and H infinity <span class="hlt">robustness</span> constraint into a more general mixed H(exp 2)/H infinity problem. No optimal solution yet is available for this more general mixed H(exp 2)/H infinity problem. Although the optimal solution for this mixed H(exp 2)/H infinity control has not yet been found, we proposed a <span class="hlt">design</span> approach which can be used through proper choice of the available <span class="hlt">design</span> parameters to influence both</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28348252','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28348252"><span>Mechanical <span class="hlt">design</span> in embryos: mechanical signalling, <span class="hlt">robustness</span> and developmental defects.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Davidson, Lance A</p> <p>2017-05-19</p> <p>Embryos are shaped by the precise application of force against the resistant structures of multicellular tissues. Forces may be generated, guided and resisted by cells, extracellular matrix, interstitial fluids, and how they are organized and bound within the tissue's architecture. In this review, we summarize our current thoughts on the multiple roles of mechanics in direct shaping, mechanical signalling and <span class="hlt">robustness</span> of development. Genetic programmes of development interact with environmental cues to direct the composition of the early embryo and endow cells with active force production. Biophysical advances now provide experimental tools to measure mechanical resistance and collective forces during morphogenesis and are allowing integration of this field with studies of signalling and patterning during development. We focus this review on concepts that highlight this integration, and how the unique contributions of mechanical cues and gradients might be tested side by side with conventional signalling systems. We conclude with speculation on the integration of large-scale programmes of development, and how mechanical responses may ensure <span class="hlt">robust</span> development and serve as constraints on programmes of tissue self-assembly.This article is part of the themed issue 'Systems morphodynamics: understanding the development of tissue hardware'. © 2017 The Author(s).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100006918','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100006918"><span>A Computational Framework to Control Verification and <span class="hlt">Robustness</span> Analysis</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Crespo, Luis G.; Kenny, Sean P.; Giesy, Daniel P.</p> <p>2010-01-01</p> <p>This paper presents a methodology for evaluating the <span class="hlt">robustness</span> of a controller based on its ability to satisfy the <span class="hlt">design</span> requirements. The framework proposed is generic since it allows for high-fidelity models, arbitrary control structures and arbitrary functional dependencies between the requirements and the uncertain parameters. The cornerstone of this contribution is the ability to bound the region of the uncertain parameter space where the degradation in closed-loop performance remains acceptable. The size of this bounding set, whose geometry can be prescribed according to deterministic or probabilistic uncertainty models, is a measure of <span class="hlt">robustness</span>. The <span class="hlt">robustness</span> metrics proposed herein are the parametric safety margin, the reliability index, the failure probability and upper bounds to this probability. The performance observed at the control verification setting, where the assumptions and approximations used for control <span class="hlt">design</span> may no longer hold, will fully determine the proposed control assessment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596976','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3596976"><span>A Unifying Mathematical Framework for Genetic <span class="hlt">Robustness</span>, Environmental <span class="hlt">Robustness</span>, Network <span class="hlt">Robustness</span> and their Trade-off on Phenotype <span class="hlt">Robustness</span> in Biological Networks Part I: Gene Regulatory Networks in Systems and Evolutionary Biology</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Chen, Bor-Sen; Lin, Ying-Po</p> <p>2013-01-01</p> <p><span class="hlt">Robust</span> stabilization and environmental disturbance attenuation are ubiquitous systematic properties observed in biological systems at different levels. The underlying principles for <span class="hlt">robust</span> stabilization and environmental disturbance attenuation are universal to both complex biological systems and sophisticated engineering systems. In many biological networks, network <span class="hlt">robustness</span> should be enough to confer intrinsic <span class="hlt">robustness</span> in order to tolerate intrinsic parameter fluctuations, genetic <span class="hlt">robustness</span> for buffering genetic variations, and environmental <span class="hlt">robustness</span> for resisting environmental disturbances. With this, the phenotypic stability of biological network can be maintained, thus guaranteeing phenotype <span class="hlt">robustness</span>. This paper presents a survey on biological systems and then develops a unifying mathematical framework for investigating the principles of both <span class="hlt">robust</span> stabilization and environmental disturbance attenuation in systems and evolutionary biology. Further, from the unifying mathematical framework, it was discovered that the phenotype <span class="hlt">robustness</span> criterion for biological networks at different levels relies upon intrinsic <span class="hlt">robustness</span> + genetic <span class="hlt">robustness</span> + environmental <span class="hlt">robustness</span> ≦ network <span class="hlt">robustness</span>. When this is true, the phenotype <span class="hlt">robustness</span> can be maintained in spite of intrinsic parameter fluctuations, genetic variations, and environmental disturbances. Therefore, the trade-offs between intrinsic <span class="hlt">robustness</span>, genetic <span class="hlt">robustness</span>, environmental <span class="hlt">robustness</span>, and network <span class="hlt">robustness</span> in systems and evolutionary biology can also be investigated through their corresponding phenotype <span class="hlt">robustness</span> criterion from the systematic point of view. PMID:23515240</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23515240','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23515240"><span>A Unifying Mathematical Framework for Genetic <span class="hlt">Robustness</span>, Environmental <span class="hlt">Robustness</span>, Network <span class="hlt">Robustness</span> and their Trade-off on Phenotype <span class="hlt">Robustness</span> in Biological Networks Part I: Gene Regulatory Networks in Systems and Evolutionary Biology.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Chen, Bor-Sen; Lin, Ying-Po</p> <p>2013-01-01</p> <p><span class="hlt">Robust</span> stabilization and environmental disturbance attenuation are ubiquitous systematic properties observed in biological systems at different levels. The underlying principles for <span class="hlt">robust</span> stabilization and environmental disturbance attenuation are universal to both complex biological systems and sophisticated engineering systems. In many biological networks, network <span class="hlt">robustness</span> should be enough to confer intrinsic <span class="hlt">robustness</span> in order to tolerate intrinsic parameter fluctuations, genetic <span class="hlt">robustness</span> for buffering genetic variations, and environmental <span class="hlt">robustness</span> for resisting environmental disturbances. With this, the phenotypic stability of biological network can be maintained, thus guaranteeing phenotype <span class="hlt">robustness</span>. This paper presents a survey on biological systems and then develops a unifying mathematical framework for investigating the principles of both <span class="hlt">robust</span> stabilization and environmental disturbance attenuation in systems and evolutionary biology. Further, from the unifying mathematical framework, it was discovered that the phenotype <span class="hlt">robustness</span> criterion for biological networks at different levels relies upon intrinsic <span class="hlt">robustness</span> + genetic <span class="hlt">robustness</span> + environmental <span class="hlt">robustness</span> ≦ network <span class="hlt">robustness</span>. When this is true, the phenotype <span class="hlt">robustness</span> can be maintained in spite of intrinsic parameter fluctuations, genetic variations, and environmental disturbances. Therefore, the trade-offs between intrinsic <span class="hlt">robustness</span>, genetic <span class="hlt">robustness</span>, environmental <span class="hlt">robustness</span>, and network <span class="hlt">robustness</span> in systems and evolutionary biology can also be investigated through their corresponding phenotype <span class="hlt">robustness</span> criterion from the systematic point of view.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://eric.ed.gov/?q=vallejo&pg=5&id=EJ762069','ERIC'); return false;" href="https://eric.ed.gov/?q=vallejo&pg=5&id=EJ762069"><span>Comparative <span class="hlt">Robustness</span> of Recent Methods for Analyzing Multivariate Repeated Measures <span class="hlt">Designs</span></span></a></p> <p><a target="_blank" href="http://www.eric.ed.gov/ERICWebPortal/search/extended.jsp?_pageLabel=advanced">ERIC Educational Resources Information Center</a></p> <p>Seco, Guillermo Vallejo; Gras, Jaime Arnau; Garcia, Manuel Ato</p> <p>2007-01-01</p> <p>This study evaluated the <span class="hlt">robustness</span> of two recent methods for analyzing multivariate repeated measures when the assumptions of covariance homogeneity and multivariate normality are violated. Specifically, the authors' work compares the performance of the modified Brown-Forsythe (MBF) procedure and the mixed-model procedure adjusted by the…</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29451086','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29451086"><span>Efficient <span class="hlt">robust</span> doubly adaptive regularized regression with applications.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Karunamuni, Rohana J; Kong, Linglong; Tu, Wei</p> <p>2018-01-01</p> <p>We consider the problem of estimation and variable selection for general linear regression models. Regularized regression procedures have been widely used for variable selection, but most existing methods perform poorly in the presence of outliers. We construct a new penalized procedure that simultaneously attains full efficiency and maximum <span class="hlt">robustness</span>. Furthermore, the proposed procedure satisfies the oracle properties. The new procedure is <span class="hlt">designed</span> to achieve sparse and <span class="hlt">robust</span> solutions by imposing adaptive weights on both the decision loss and the penalty function. The proposed method of estimation and variable selection attains full efficiency when the model is correct and, at the same time, achieves maximum <span class="hlt">robustness</span> when outliers are present. We examine the <span class="hlt">robustness</span> properties using the finite-sample breakdown point and an influence function. We show that the proposed estimator attains the maximum breakdown point. Furthermore, there is no loss in efficiency when there are no outliers or the error distribution is normal. For practical implementation of the proposed method, we present a computational algorithm. We examine the finite-sample and <span class="hlt">robustness</span> properties using Monte Carlo studies. Two datasets are also analyzed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19900000643&hterms=least+squares&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dleast%2Bsquares','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19900000643&hterms=least+squares&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dleast%2Bsquares"><span>Software For Least-Squares And <span class="hlt">Robust</span> Estimation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Jeffreys, William H.; Fitzpatrick, Michael J.; Mcarthur, Barbara E.; Mccartney, James</p> <p>1990-01-01</p> <p>GAUSSFIT computer program includes full-featured programming language facilitating creation of mathematical models solving least-squares and <span class="hlt">robust</span>-estimation problems. Programming language <span class="hlt">designed</span> to make it easy to specify complex reduction models. Written in 100 percent C language.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23735558','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23735558"><span><span class="hlt">Robust</span> hopping based on virtual pendulum posture control.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sharbafi, Maziar A; Maufroy, Christophe; Ahmadabadi, Majid Nili; Yazdanpanah, Mohammad J; Seyfarth, Andre</p> <p>2013-09-01</p> <p>A new control approach to achieve <span class="hlt">robust</span> hopping against perturbations in the sagittal plane is presented in this paper. In perturbed hopping, vertical body alignment has a significant role for stability. Our approach is based on the virtual pendulum concept, recently proposed, based on experimental findings in human and animal locomotion. In this concept, the ground reaction forces are pointed to a virtual support point, named virtual pivot point (VPP), during motion. This concept is employed in <span class="hlt">designing</span> the controller to balance the trunk during the stance phase. New strategies for leg angle and length adjustment besides the virtual pendulum posture control are proposed as a unified controller. This method is investigated by applying it on an extension of the spring loaded inverted pendulum (SLIP) model. Trunk, leg mass and damping are added to the SLIP model in order to make the model more realistic. The stability is analyzed by Poincaré map analysis. With fixed VPP position, stability, disturbance rejection and moderate <span class="hlt">robustness</span> are achieved, but with a low convergence speed. To improve the performance and attain higher <span class="hlt">robustness</span>, an event-based control of the VPP position is introduced, using feedback of the system states at apexes. Discrete linear quartic regulator is used to <span class="hlt">design</span> the feedback controller. Considerable enhancements with respect to stability, convergence speed and <span class="hlt">robustness</span> against perturbations and parameter changes are achieved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017VSD....55.1189M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017VSD....55.1189M"><span><span class="hlt">Robustness</span> analysis of bogie suspension components Pareto optimised values</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mousavi Bideleh, Seyed Milad</p> <p>2017-08-01</p> <p>Bogie suspension system of high speed trains can significantly affect vehicle performance. Multiobjective optimisation problems are often formulated and solved to find the Pareto optimised values of the suspension components and improve cost efficiency in railway operations from different perspectives. Uncertainties in the <span class="hlt">design</span> parameters of suspension system can negatively influence the dynamics behaviour of railway vehicles. In this regard, <span class="hlt">robustness</span> analysis of a bogie dynamics response with respect to uncertainties in the suspension <span class="hlt">design</span> parameters is considered. A one-car railway vehicle model with 50 degrees of freedom and wear/comfort Pareto optimised values of bogie suspension components is chosen for the analysis. Longitudinal and lateral primary stiffnesses, longitudinal and vertical secondary stiffnesses, as well as yaw damping are considered as five <span class="hlt">design</span> parameters. The effects of parameter uncertainties on wear, ride comfort, track shift force, stability, and risk of derailment are studied by varying the <span class="hlt">design</span> parameters around their respective Pareto optimised values according to a lognormal distribution with different coefficient of variations (COVs). The <span class="hlt">robustness</span> analysis is carried out based on the maximum entropy concept. The multiplicative dimensional reduction method is utilised to simplify the calculation of fractional moments and improve the computational efficiency. The results showed that the dynamics response of the vehicle with wear/comfort Pareto optimised values of bogie suspension is <span class="hlt">robust</span> against uncertainties in the <span class="hlt">design</span> parameters and the probability of failure is small for parameter uncertainties with COV up to 0.1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018IJSS...49..511S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018IJSS...49..511S"><span><span class="hlt">Robust</span> approximation-free prescribed performance control for nonlinear systems and its application</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sun, Ruisheng; Na, Jing; Zhu, Bin</p> <p>2018-02-01</p> <p>This paper presents a <span class="hlt">robust</span> prescribed performance control approach and its application to nonlinear tail-controlled missile systems with unknown dynamics and uncertainties. The idea of prescribed performance function (PPF) is incorporated into the control <span class="hlt">design</span>, such that both the steady-state and transient control performance can be strictly guaranteed. Unlike conventional PPF-based control methods, we further tailor a recently proposed systematic control <span class="hlt">design</span> procedure (i.e. approximation-free control) using the transformed tracking error dynamics, which provides a proportional-like control action. Hence, the function approximators (e.g. neural networks, fuzzy systems) that are widely used to address the unknown nonlinearities in the nonlinear control <span class="hlt">designs</span> are not needed. The proposed control <span class="hlt">design</span> leads to a <span class="hlt">robust</span> yet simplified function approximation-free control for nonlinear systems. The closed-loop system stability and the control error convergence are all rigorously proved. Finally, comparative simulations are conducted based on nonlinear missile systems to validate the improved response and the <span class="hlt">robustness</span> of the proposed control method.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4477258','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4477258"><span>A <span class="hlt">Robust</span> H ∞ Controller for an UAV Flight Control System</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>López, J.</p> <p>2015-01-01</p> <p>The objective of this paper is the implementation and validation of a <span class="hlt">robust</span> H ∞ controller for an UAV to track all types of manoeuvres in the presence of noisy environment. A <span class="hlt">robust</span> inner-outer loop strategy is implemented. To <span class="hlt">design</span> the H ∞ <span class="hlt">robust</span> controller in the inner loop, H ∞ control methodology is used. The two controllers that conform the outer loop are <span class="hlt">designed</span> using the H ∞ Loop Shaping technique. The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft. The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements. PMID:26221622</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26221622','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26221622"><span>A <span class="hlt">Robust</span> H ∞ Controller for an UAV Flight Control System.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>López, J; Dormido, R; Dormido, S; Gómez, J P</p> <p>2015-01-01</p> <p>The objective of this paper is the implementation and validation of a <span class="hlt">robust</span> H ∞ controller for an UAV to track all types of manoeuvres in the presence of noisy environment. A <span class="hlt">robust</span> inner-outer loop strategy is implemented. To <span class="hlt">design</span> the H ∞ <span class="hlt">robust</span> controller in the inner loop, H ∞ control methodology is used. The two controllers that conform the outer loop are <span class="hlt">designed</span> using the H ∞ Loop Shaping technique. The reference vector used in the control architecture formed by vertical velocity, true airspeed, and heading angle, suggests a nontraditional way to pilot the aircraft. The simulation results show that the proposed control scheme works well despite the presence of noise and uncertainties, so the control system satisfies the requirements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JMEP...24.4870L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JMEP...24.4870L"><span>Improved Stress Corrosion Cracking Resistance and Strength of a Two-Step Aged Al-Zn-Mg-Cu Alloy Using <span class="hlt">Taguchi</span> Method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lin, Lianghua; Liu, Zhiyi; Ying, Puyou; Liu, Meng</p> <p>2015-12-01</p> <p>Multi-step heat treatment effectively enhances the stress corrosion cracking (SCC) resistance but usually degrades the mechanical properties of Al-Zn-Mg-Cu alloys. With the aim to enhance SCC resistance as well as strength of Al-Zn-Mg-Cu alloys, we have optimized the process parameters during two-step aging of Al-6.1Zn-2.8Mg-1.9Cu alloy by <span class="hlt">Taguchi</span>'s L9 orthogonal array. In this work, analysis of variance (ANOVA) was performed to find out the significant heat treatment parameters. The slow strain rate testing combined with scanning electron microscope and transmission electron microscope was employed to study the SCC behaviors of Al-Zn-Mg-Cu alloy. Results showed that the contour map produced by ANOVA offered a reliable reference for selection of optimum heat treatment parameters. By using this method, a desired combination of mechanical performances and SCC resistance was obtained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010SPIE.7698E..0AC','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010SPIE.7698E..0AC"><span>Optimization of a chemical identification algorithm</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chyba, Thomas H.; Fisk, Brian; Gunning, Christin; Farley, Kevin; Polizzi, Amber; Baughman, David; Simpson, Steven; Slamani, Mohamed-Adel; Almassy, Robert; Da Re, Ryan; Li, Eunice; MacDonald, Steve; Slamani, Ahmed; Mitchell, Scott A.; Pendell-Jones, Jay; Reed, Timothy L.; Emge, Darren</p> <p>2010-04-01</p> <p>A procedure to evaluate and optimize the performance of a chemical identification algorithm is presented. The Joint Contaminated Surface Detector (JCSD) employs Raman spectroscopy to detect and identify surface chemical contamination. JCSD measurements of chemical warfare agents, simulants, toxic industrial chemicals, interferents and bare surface backgrounds were made in the laboratory and under realistic field conditions. A test data suite, developed from these measurements, is used to benchmark algorithm performance throughout the improvement process. In any one measurement, one of many possible targets can be present along with interferents and surfaces. The detection results are expressed as a 2-category classification problem so that Receiver Operating Characteristic (ROC) techniques can be applied. The limitations of applying this framework to chemical detection problems are discussed along with means to mitigate them. Algorithmic performance is optimized globally using <span class="hlt">robust</span> <span class="hlt">Design</span> of Experiments and <span class="hlt">Taguchi</span> techniques. These methods require figures of merit to trade off between false alarms and detection probability. Several figures of merit, including the Matthews Correlation Coefficient and the <span class="hlt">Taguchi</span> Signal-to-Noise Ratio are compared. Following the optimization of global parameters which govern the algorithm behavior across all target chemicals, ROC techniques are employed to optimize chemical-specific parameters to further improve performance.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017SMaS...26c5056Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017SMaS...26c5056Y"><span><span class="hlt">Robust</span> control of seismically excited cable stayed bridges with MR dampers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>YeganehFallah, Arash; Khajeh Ahamd Attari, Nader</p> <p>2017-03-01</p> <p>In recent decades active and semi-active structural control are becoming attractive alternatives for enhancing performance of civil infrastructures subjected to seismic and winds loads. However, in order to have reliable active and semi-active control, there is a need to include information of uncertainties in <span class="hlt">design</span> of the controller. In real world for civil structures, parameters such as loading places, stiffness, mass and damping are time variant and uncertain. These uncertainties in many cases model as parametric uncertainties. The motivation of this research is to <span class="hlt">design</span> a <span class="hlt">robust</span> controller for attenuating the vibrational responses of civil infrastructures, regarding their dynamical uncertainties. Uncertainties in structural dynamic’s parameters are modeled as affine uncertainties in state space modeling. These uncertainties are decoupled from the system through Linear Fractional Transformation (LFT) and are assumed to be unknown input to the system but norm bounded. The <span class="hlt">robust</span> H ∞ controller is <span class="hlt">designed</span> for the decoupled system to regulate the evaluation outputs and it is <span class="hlt">robust</span> to effects of uncertainties, disturbance and sensors noise. The cable stayed bridge benchmark which is equipped with MR damper is considered for the numerical simulation. The simulated results show that the proposed <span class="hlt">robust</span> controller can effectively mitigate undesired uncertainties effects on systems’ responds under seismic loading.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_24 --> <div id="page_25" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="481"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017IJC....90.2449Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017IJC....90.2449Z"><span><span class="hlt">Robust</span> distributed model predictive control of linear systems with structured time-varying uncertainties</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Langwen; Xie, Wei; Wang, Jingcheng</p> <p>2017-11-01</p> <p>In this work, synthesis of <span class="hlt">robust</span> distributed model predictive control (MPC) is presented for a class of linear systems subject to structured time-varying uncertainties. By decomposing a global system into smaller dimensional subsystems, a set of distributed MPC controllers, instead of a centralised controller, are <span class="hlt">designed</span>. To ensure the <span class="hlt">robust</span> stability of the closed-loop system with respect to model uncertainties, distributed state feedback laws are obtained by solving a min-max optimisation problem. The <span class="hlt">design</span> of <span class="hlt">robust</span> distributed MPC is then transformed into solving a minimisation optimisation problem with linear matrix inequality constraints. An iterative online algorithm with adjustable maximum iteration is proposed to coordinate the distributed controllers to achieve a global performance. The simulation results show the effectiveness of the proposed <span class="hlt">robust</span> distributed MPC algorithm.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20000032579','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20000032579"><span><span class="hlt">Robust</span> Control of Uncertain Systems via Dissipative LQG-Type Controllers</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Joshi, Suresh M.</p> <p>2000-01-01</p> <p>Optimal controller <span class="hlt">design</span> is addressed for a class of linear, time-invariant systems which are dissipative with respect to a quadratic power function. The system matrices are assumed to be affine functions of uncertain parameters confined to a convex polytopic region in the parameter space. For such systems, a method is developed for <span class="hlt">designing</span> a controller which is dissipative with respect to a given power function, and is simultaneously optimal in the linear-quadratic-Gaussian (LQG) sense. The resulting controller provides <span class="hlt">robust</span> stability as well as optimal performance. Three important special cases, namely, passive, norm-bounded, and sector-bounded controllers, which are also LQG-optimal, are presented. The results give new methods for <span class="hlt">robust</span> controller <span class="hlt">design</span> in the presence of parametric uncertainties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920074617&hterms=Costs+operation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DCosts%2Boperation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920074617&hterms=Costs+operation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DCosts%2Boperation"><span>The importance of operations, risk, and cost assessment to space transfer systems <span class="hlt">design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ball, J. M.; Komerska, R. J.; Rowell, L. F.</p> <p>1992-01-01</p> <p>This paper examines several methodologies which contribute to comprehensive subsystem cost estimation. The example of a space-based lunar space transfer vehicle (STV) <span class="hlt">design</span> is used to illustrate how including both primary and secondary factors into cost affects the decision of whether to use aerobraking or propulsion for earth orbit capture upon lunar return. The expected dominant cost factor in this decision is earth-to-orbit launch cost driven by STV mass. However, to quantify other significant cost factors, this cost comparison included a risk analysis to identify development and testing costs, a <span class="hlt">Taguchi</span> <span class="hlt">design</span> of experiments to determine a minimum mass aerobrake <span class="hlt">design</span>, and a detailed operations analysis. As a result, the predicted cost advantage of aerobraking, while still positive, was subsequently reduced by about 30 percent compared to the simpler mass-based cost estimates.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28945071','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28945071"><span>A Triblock Copolymer <span class="hlt">Design</span> Leads to <span class="hlt">Robust</span> Hybrid Hydrogels for High-Performance Flexible Supercapacitors.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zhang, Guangzhao; Chen, Yunhua; Deng, Yonghong; Wang, Chaoyang</p> <p>2017-10-18</p> <p>We report here an intriguing hybrid conductive hydrogel as electrode for high-performance flexible supercapacitor. The key is using a rationally <span class="hlt">designed</span> water-soluble ABA triblock copolymer (termed as IAOAI) containing a central poly(ethylene oxide) block (A) and terminal poly(acrylamide) (PAAm) block with aniline moieties randomly incorporated (B), which was synthesized by reversible additional fragment transfer polymerization. The subsequent copolymerization of aniline monomers with the terminated aniline moieties on the IAOAI polymer generates a three-dimensional cross-linking hybrid network. The hybrid hydrogel electrode demonstrates <span class="hlt">robust</span> mechanical flexibility, remarkable electrochemical capacitance (919 F/g), and cyclic stability (90% capacitance retention after 1000 cycles). Moreover, the flexible supercapacitor based on this hybrid hydrogel electrode presents a large specific capacitance (187 F/g), superior to most reported conductive hydrogel-based supercapacitors. With the demonstrated additional favorable cyclic stability and excellent capacitive and rate performance, this hybrid hydrogel-based supercapacitor holds great promise for flexible energy-storage device.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=128573','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=128573"><span>Complexity and <span class="hlt">robustness</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Carlson, J. M.; Doyle, John</p> <p>2002-01-01</p> <p>Highly optimized tolerance (HOT) was recently introduced as a conceptual framework to study fundamental aspects of complexity. HOT is motivated primarily by systems from biology and engineering and emphasizes, (i) highly structured, nongeneric, self-dissimilar internal configurations, and (ii) <span class="hlt">robust</span> yet fragile external behavior. HOT claims these are the most important features of complexity and not accidents of evolution or artifices of engineering <span class="hlt">design</span> but are inevitably intertwined and mutually reinforcing. In the spirit of this collection, our paper contrasts HOT with alternative perspectives on complexity, drawing on real-world examples and also model systems, particularly those from self-organized criticality. PMID:11875207</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21855061','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21855061"><span><span class="hlt">Robust</span> <span class="hlt">design</span> of a 2-DOF GMV controller: a direct self-tuning and fuzzy scheduling approach.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Silveira, Antonio S; Rodríguez, Jaime E N; Coelho, Antonio A R</p> <p>2012-01-01</p> <p>This paper presents a study on self-tuning control strategies with generalized minimum variance control in a fixed two degree of freedom structure-or simply GMV2DOF-within two adaptive perspectives. One, from the process model point of view, using a recursive least squares estimator algorithm for direct self-tuning <span class="hlt">design</span>, and another, using a Mamdani fuzzy GMV2DOF parameters scheduling technique based on analytical and physical interpretations from <span class="hlt">robustness</span> analysis of the system. Both strategies are assessed by simulation and real plants experimentation environments composed of a damped pendulum and an under development wind tunnel from the Department of Automation and Systems of the Federal University of Santa Catarina. Copyright © 2011 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ApPhA.123..230B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ApPhA.123..230B"><span>Surface laser marking optimization using an experimental <span class="hlt">design</span> approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Brihmat-Hamadi, F.; Amara, E. H.; Lavisse, L.; Jouvard, J. M.; Cicala, E.; Kellou, H.</p> <p>2017-04-01</p> <p>Laser surface marking is performed on a titanium substrate using a pulsed frequency doubled Nd:YAG laser ( λ= 532 nm, τ pulse=5 ns) to process the substrate surface under normal atmospheric conditions. The aim of the work is to investigate, following experimental and statistical approaches, the correlation between the process parameters and the response variables (output), using a <span class="hlt">Design</span> of Experiment method (DOE): <span class="hlt">Taguchi</span> methodology and a response surface methodology (RSM). A <span class="hlt">design</span> is first created using MINTAB program, and then the laser marking process is performed according to the planned <span class="hlt">design</span>. The response variables; surface roughness and surface reflectance were measured for each sample, and incorporated into the <span class="hlt">design</span> matrix. The results are then analyzed and the RSM model is developed and verified for predicting the process output for the given set of process parameters values. The analysis shows that the laser beam scanning speed is the most influential operating factor followed by the laser pumping intensity during marking, while the other factors show complex influences on the objective functions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009LNCS.5874...24D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009LNCS.5874...24D"><span>Evaluation of Recoverable-<span class="hlt">Robust</span> Timetables on Tree Networks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>D'Angelo, Gianlorenzo; di Stefano, Gabriele; Navarra, Alfredo</p> <p></p> <p>In the context of scheduling and timetabling, we study a challenging combinatorial problem which is interesting from both a practical and a theoretical point of view. The motivation behind it is to cope with scheduled activities which might be subject to unavoidable disturbances, such as delays, occurring during the operational phase. The idea is to preventively plan some extra time for the scheduled activities in order to be "prepared" if a delay occurs, and to absorb it without the necessity of re-scheduling the activities from scratch. This realizes the concept of <span class="hlt">designing</span> so called <span class="hlt">robust</span> timetables. During the planning phase, one has to consider recovery features that might be applied at runtime if delays occur. Such recovery capabilities are given as input along with the possible delays that must be considered. The objective is the minimization of the overall needed time. The quality of a <span class="hlt">robust</span> timetable is measured by the price of <span class="hlt">robustness</span>, i.e. the ratio between the cost of the <span class="hlt">robust</span> timetable and that of a non-<span class="hlt">robust</span> optimal timetable. The considered problem is known to be NP-hard. We propose a pseudo-polynomial time algorithm and apply it on random networks and real case scenarios provided by Italian railways. We evaluate the effect of <span class="hlt">robustness</span> on the scheduling of the activities and provide the price of <span class="hlt">robustness</span> with respect to different scenarios. We experimentally show the practical effectiveness and efficiency of the proposed algorithm.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1375170','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1375170"><span>Examining <span class="hlt">robustness</span> of model selection with half-normal and LASSO plots for unreplicated factorial <span class="hlt">designs</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Jang, Dae -Heung; Anderson-Cook, Christine Michaela</p> <p></p> <p>When there are constraints on resources, an unreplicated factorial or fractional factorial <span class="hlt">design</span> can allow efficient exploration of numerous factor and interaction effects. A half-normal plot is a common graphical tool used to compare the relative magnitude of effects and to identify important effects from these experiments when no estimate of error from the experiment is available. An alternative is to use a least absolute shrinkage and selection operation plot to examine the pattern of model selection terms from an experiment. We examine how both the half-normal and least absolute shrinkage and selection operation plots are impacted by the absencemore » of individual observations or an outlier, and the <span class="hlt">robustness</span> of conclusions obtained from these 2 techniques for identifying important effects from factorial experiments. As a result, the methods are illustrated with 2 examples from the literature.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1375170-examining-robustness-model-selection-half-normal-lasso-plots-unreplicated-factorial-designs','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1375170-examining-robustness-model-selection-half-normal-lasso-plots-unreplicated-factorial-designs"><span>Examining <span class="hlt">robustness</span> of model selection with half-normal and LASSO plots for unreplicated factorial <span class="hlt">designs</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Jang, Dae -Heung; Anderson-Cook, Christine Michaela</p> <p>2017-04-12</p> <p>When there are constraints on resources, an unreplicated factorial or fractional factorial <span class="hlt">design</span> can allow efficient exploration of numerous factor and interaction effects. A half-normal plot is a common graphical tool used to compare the relative magnitude of effects and to identify important effects from these experiments when no estimate of error from the experiment is available. An alternative is to use a least absolute shrinkage and selection operation plot to examine the pattern of model selection terms from an experiment. We examine how both the half-normal and least absolute shrinkage and selection operation plots are impacted by the absencemore » of individual observations or an outlier, and the <span class="hlt">robustness</span> of conclusions obtained from these 2 techniques for identifying important effects from factorial experiments. As a result, the methods are illustrated with 2 examples from the literature.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960003340','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960003340"><span><span class="hlt">Robust</span> stability of second-order systems</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chuang, C.-H.</p> <p>1995-01-01</p> <p>It has been shown recently how virtual passive controllers can be <span class="hlt">designed</span> for second-order dynamic systems to achieve <span class="hlt">robust</span> stability. The virtual controllers were visualized as systems made up of spring, mass and damping elements. In this paper, a new approach emphasizing on the notion of positive realness to the same second-order dynamic systems is used. Necessary and sufficient conditions for positive realness are presented for scalar spring-mass-dashpot systems. For multi-input multi-output systems, we show how a mass-spring-dashpot system can be made positive real by properly choosing its output variables. In particular, sufficient conditions are shown for the system without output velocity. Furthermore, if velocity cannot be measured then the system parameters must be precise to keep the system positive real. In practice, system parameters are not always constant and cannot be measured precisely. Therefore, in order to be useful positive real systems must be <span class="hlt">robust</span> to some degrees. This can be achieved with the <span class="hlt">design</span> presented in this paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3969875','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3969875"><span><span class="hlt">Robust</span> Mediation Analysis Based on Median Regression</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Yuan, Ying; MacKinnon, David P.</p> <p>2014-01-01</p> <p>Mediation analysis has many applications in psychology and the social sciences. The most prevalent methods typically assume that the error distribution is normal and homoscedastic. However, this assumption may rarely be met in practice, which can affect the validity of the mediation analysis. To address this problem, we propose <span class="hlt">robust</span> mediation analysis based on median regression. Our approach is <span class="hlt">robust</span> to various departures from the assumption of homoscedasticity and normality, including heavy-tailed, skewed, contaminated, and heteroscedastic distributions. Simulation studies show that under these circumstances, the proposed method is more efficient and powerful than standard mediation analysis. We further extend the proposed <span class="hlt">robust</span> method to multilevel mediation analysis, and demonstrate through simulation studies that the new approach outperforms the standard multilevel mediation analysis. We illustrate the proposed method using data from a program <span class="hlt">designed</span> to increase reemployment and enhance mental health of job seekers. PMID:24079925</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27538818','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27538818"><span>A <span class="hlt">robust</span> two-stage <span class="hlt">design</span> identifying the optimal biological dose for phase I/II clinical trials.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zang, Yong; Lee, J Jack</p> <p>2017-01-15</p> <p>We propose a <span class="hlt">robust</span> two-stage <span class="hlt">design</span> to identify the optimal biological dose for phase I/II clinical trials evaluating both toxicity and efficacy outcomes. In the first stage of dose finding, we use the Bayesian model averaging continual reassessment method to monitor the toxicity outcomes and adopt an isotonic regression method based on the efficacy outcomes to guide dose escalation. When the first stage ends, we use the Dirichlet-multinomial distribution to jointly model the toxicity and efficacy outcomes and pick the candidate doses based on a three-dimensional volume ratio. The selected candidate doses are then seamlessly advanced to the second stage for dose validation. Both toxicity and efficacy outcomes are continuously monitored so that any overly toxic and/or less efficacious dose can be dropped from the study as the trial continues. When the phase I/II trial ends, we select the optimal biological dose as the dose obtaining the minimal value of the volume ratio within the candidate set. An advantage of the proposed <span class="hlt">design</span> is that it does not impose a monotonically increasing assumption on the shape of the dose-efficacy curve. We conduct extensive simulation studies to examine the operating characteristics of the proposed <span class="hlt">design</span>. The simulation results show that the proposed <span class="hlt">design</span> has desirable operating characteristics across different shapes of the underlying true dose-toxicity and dose-efficacy curves. The software to implement the proposed <span class="hlt">design</span> is available upon request. Copyright © 2016 John Wiley & Sons, Ltd. Copyright © 2016 John Wiley & Sons, Ltd.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012SuMi...52.1131Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012SuMi...52.1131Y"><span>The structure and photocatalytic activity of TiO2 thin films deposited by dc magnetron sputtering</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, W. J.; Hsu, C. Y.; Liu, Y. W.; Hsu, R. Q.; Lu, T. W.; Hu, C. C.</p> <p>2012-12-01</p> <p>This paper seeks to determine the optimal settings for the deposition parameters, for TiO2 thin film, prepared on non-alkali glass substrates, by direct current (dc) sputtering, using a ceramic TiO2 target in an argon gas environment. An orthogonal array, the signal-to-noise ratio and analysis of variance are used to analyze the effect of the deposition parameters. Using the <span class="hlt">Taguchi</span> method for <span class="hlt">design</span> of a <span class="hlt">robust</span> experiment, the interactions between factors are also investigated. The main deposition parameters, such as dc power (W), sputtering pressure (Pa), substrate temperature (°C) and deposition time (min), were optimized, with reference to the structure and photocatalytic characteristics of TiO2. The results of this study show that substrate temperature and deposition time have the most significant effect on photocatalytic performance. For the optimal combination of deposition parameters, the (1 1 0) and (2 0 0) peaks of the rutile structure and the (2 0 0) peak of the anatase structure were observed, at 2θ ˜ 27.4°, 39.2° and 48°, respectively. The experimental results illustrate that the <span class="hlt">Taguchi</span> method allowed a suitable solution to the problem, with the minimum number of trials, compared to a full factorial <span class="hlt">design</span>. The adhesion of the coatings was also measured and evaluated, via a scratch test. Superior wear behavior was observed, for the TiO2 film, because of the increased strength of the interface of micro-blasted tools.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21801482','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21801482"><span>Stability-indicating LC assay for butenafine hydrochloride in creams using an experimental <span class="hlt">design</span> for <span class="hlt">robustness</span> evaluation and photodegradation kinetics study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Barth, Aline Bergesch; de Oliveira, Gabriela Bolfe; Malesuik, Marcelo Donadel; Paim, Clésio Soldatelli; Volpato, Nadia Maria</p> <p>2011-08-01</p> <p>A stability-indicating liquid chromatography method for the determination of the antifungal agent butenafine hydrochloride (BTF) in a cream was developed and validated using the Plackett-Burman experimental <span class="hlt">design</span> for <span class="hlt">robustness</span> evaluation. Also, the drug photodegradation kinetics was determined. The analytical column was operated with acetonitrile, methanol and a solution of triethylamine 0.3% adjusted to pH 4.0 (6:3:1) at a flow rate of 1 mL/min and detection at 283 nm. BTF extraction from the cream was done with n-butyl alcohol and methanol in ultrasonic bath. The performed degradation conditions were: acid and basic media with HCl 1M and NaOH 1M, respectively, oxidation with H(2)O(2) 10%, and the exposure to UV-C light. No interference in the BTF elution was verified. Linearity was assessed (r(2) = 0.9999) and ANOVA showed non-significative linearity deviation (p > 0.05). Adequate results were obtained for repeatability, intra-day precision, and accuracy. Critical factors were selected to examine the method <span class="hlt">robustness</span> with the two-level Plackett-Burman experimental <span class="hlt">design</span> and no significant factors were detected (p > 0.05). The BTF photodegradation kinetics was determined for the standard and for the cream, both in methanolic solution, under UV light at 254 nm. The degradation process can be described by first-order kinetics in both cases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhyA..446...82S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhyA..446...82S"><span>Tabu Search enhances network <span class="hlt">robustness</span> under targeted attacks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sun, Shi-wen; Ma, Yi-lin; Li, Rui-qi; Wang, Li; Xia, Cheng-yi</p> <p>2016-03-01</p> <p>We focus on the optimization of network <span class="hlt">robustness</span> with respect to intentional attacks on high-degree nodes. Given an existing network, this problem can be considered as a typical single-objective combinatorial optimization problem. Based on the heuristic Tabu Search optimization algorithm, a link-rewiring method is applied to reconstruct the network while keeping the degree of every node unchanged. Through numerical simulations, BA scale-free network and two real-world networks are investigated to verify the effectiveness of the proposed optimization method. Meanwhile, we analyze how the optimization affects other topological properties of the networks, including natural connectivity, clustering coefficient and degree-degree correlation. The current results can help to improve the <span class="hlt">robustness</span> of existing complex real-world systems, as well as to provide some insights into the <span class="hlt">design</span> of <span class="hlt">robust</span> networks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120011893','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120011893"><span><span class="hlt">Robust</span> Tensioned Kevlar Suspension <span class="hlt">Design</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Young, Joseph B.; Naylor, Bret J.; Holmes, Warren A.</p> <p>2012-01-01</p> <p>One common but challenging problem in cryogenic engineering is to produce a mount that has excellent thermal isolation but is also rigid. Such mounts can be achieved by suspending the load from a network of fibers or strings held in tension. Kevlar fibers are often used for this purpose owing to their high strength and low thermal conductivity. A suite of compact <span class="hlt">design</span> elements has been developed to improve the reliability of suspension systems made of Kevlar.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28153542','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28153542"><span>Adaptive integral <span class="hlt">robust</span> control and application to electromechanical servo systems.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Deng, Wenxiang; Yao, Jianyong</p> <p>2017-03-01</p> <p>This paper proposes a continuous adaptive integral <span class="hlt">robust</span> control with <span class="hlt">robust</span> integral of the sign of the error (RISE) feedback for a class of uncertain nonlinear systems, in which the RISE feedback gain is adapted online to ensure the <span class="hlt">robustness</span> against disturbances without the prior bound knowledge of the additive disturbances. In addition, an adaptive compensation integrated with the proposed adaptive RISE feedback term is also constructed to further reduce <span class="hlt">design</span> conservatism when the system also exists parametric uncertainties. Lyapunov analysis reveals the proposed controllers could guarantee the tracking errors are asymptotically converging to zero with continuous control efforts. To illustrate the high performance nature of the developed controllers, numerical simulations are provided. At the end, an application case of an actual electromechanical servo system driven by motor is also studied, with some specific <span class="hlt">design</span> consideration, and comparative experimental results are obtained to verify the effectiveness of the proposed controllers. Copyright © 2017 ISA. Published by Elsevier Ltd. All rights reserved.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JAP...120f5304M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JAP...120f5304M"><span>Synthesis of graphene by cobalt-catalyzed decomposition of methane in plasma-enhanced CVD: Optimization of experimental parameters with <span class="hlt">Taguchi</span> method</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mehedi, H.-A.; Baudrillart, B.; Alloyeau, D.; Mouhoub, O.; Ricolleau, C.; Pham, V. D.; Chacon, C.; Gicquel, A.; Lagoute, J.; Farhat, S.</p> <p>2016-08-01</p> <p>This article describes the significant roles of process parameters in the deposition of graphene films via cobalt-catalyzed decomposition of methane diluted in hydrogen using plasma-enhanced chemical vapor deposition (PECVD). The influence of growth temperature (700-850 °C), molar concentration of methane (2%-20%), growth time (30-90 s), and microwave power (300-400 W) on graphene thickness and defect density is investigated using <span class="hlt">Taguchi</span> method which enables reaching the optimal parameter settings by performing reduced number of experiments. Growth temperature is found to be the most influential parameter in minimizing the number of graphene layers, whereas microwave power has the second largest effect on crystalline quality and minor role on thickness of graphene films. The structural properties of PECVD graphene obtained with optimized synthesis conditions are investigated with Raman spectroscopy and corroborated with atomic-scale characterization performed by high-resolution transmission electron microscopy and scanning tunneling microscopy, which reveals formation of continuous film consisting of 2-7 high quality graphene layers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015PMB....60.2671M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015PMB....60.2671M"><span>Defining <span class="hlt">robustness</span> protocols: a method to include and evaluate <span class="hlt">robustness</span> in clinical plans</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>McGowan, S. E.; Albertini, F.; Thomas, S. J.; Lomax, A. J.</p> <p>2015-04-01</p> <p>We aim to define a site-specific <span class="hlt">robustness</span> protocol to be used during the clinical plan evaluation process. Plan <span class="hlt">robustness</span> of 16 skull base IMPT plans to systematic range and random set-up errors have been retrospectively and systematically analysed. This was determined by calculating the error-bar dose distribution (ebDD) for all the plans and by defining some metrics used to define protocols aiding the plan assessment. Additionally, an example of how to clinically use the defined <span class="hlt">robustness</span> database is given whereby a plan with sub-optimal brainstem <span class="hlt">robustness</span> was identified. The advantage of using different beam arrangements to improve the plan <span class="hlt">robustness</span> was analysed. Using the ebDD it was found range errors had a smaller effect on dose distribution than the corresponding set-up error in a single fraction, and that organs at risk were most <span class="hlt">robust</span> to the range errors, whereas the target was more <span class="hlt">robust</span> to set-up errors. A database was created to aid planners in terms of plan <span class="hlt">robustness</span> aims in these volumes. This resulted in the definition of site-specific <span class="hlt">robustness</span> protocols. The use of <span class="hlt">robustness</span> constraints allowed for the identification of a specific patient that may have benefited from a treatment of greater individuality. A new beam arrangement showed to be preferential when balancing conformality and <span class="hlt">robustness</span> for this case. The ebDD and error-bar volume histogram proved effective in analysing plan <span class="hlt">robustness</span>. The process of retrospective analysis could be used to establish site-specific <span class="hlt">robustness</span> planning protocols in proton therapy. These protocols allow the planner to determine plans that, although delivering a dosimetrically adequate dose distribution, have resulted in sub-optimal <span class="hlt">robustness</span> to these uncertainties. For these cases the use of different beam start conditions may improve the plan <span class="hlt">robustness</span> to set-up and range uncertainties.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_25 --> <div class="footer-extlink text-muted" style="margin-bottom:1rem; text-align:center;">Some links on this page may take you to non-federal websites. 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